Procedure Acquisition List
Get a list of ProcedureAcquisition objects. ProcedureAcquisitions have a 1:1 mapping with Observations.
GET /api/v3/acquisitions/?format=api&offset=2200
{ "count": 5833, "next": "https://api.catalogue.ceda.ac.uk/api/v3/acquisitions/?format=api&limit=100&offset=2300", "previous": "https://api.catalogue.ceda.ac.uk/api/v3/acquisitions/?format=api&limit=100&offset=2100", "results": [ { "ob_id": 9966, "uuid": "14a87e6740ff40db961785880a215b01", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 85/CR1 over the Morfa Mawr, Plas Gogerddan and Bronydd Mawr Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3231, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 9966, "uuid": "14a87e6740ff40db961785880a215b01", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 85/CR1 over the Morfa Mawr, Plas Gogerddan and Bronydd Mawr Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3232, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 9966, "uuid": "14a87e6740ff40db961785880a215b01", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 85/CR1 over the Morfa Mawr, Plas Gogerddan and Bronydd Mawr Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 9970, "uuid": "14dd7696ced84c90bf84db3d3bb90147", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/01 over the Loch Assynt Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3233, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 9970, "uuid": "14dd7696ced84c90bf84db3d3bb90147", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/01 over the Loch Assynt Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3234, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 9970, "uuid": "14dd7696ced84c90bf84db3d3bb90147", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/01 over the Loch Assynt Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 9974, "uuid": "ce4c3834f4724e6da6ed2537956e4514", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/02 over the Lathkill Dale Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3235, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 9974, "uuid": "ce4c3834f4724e6da6ed2537956e4514", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/02 over the Lathkill Dale Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3236, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 9974, "uuid": "ce4c3834f4724e6da6ed2537956e4514", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/02 over the Lathkill Dale Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 9978, "uuid": "e5d08d09f34f4ec99a8ac8023af8de98", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/03 over the Danby High Moor Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3237, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 9978, "uuid": "e5d08d09f34f4ec99a8ac8023af8de98", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/03 over the Danby High Moor Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3238, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 9978, "uuid": "e5d08d09f34f4ec99a8ac8023af8de98", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/03 over the Danby High Moor Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 9982, "uuid": "7f5c31b4d9f74e81bde883596bb7d79c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/04 over the Sutton Bonington Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3239, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 9982, "uuid": "7f5c31b4d9f74e81bde883596bb7d79c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/04 over the Sutton Bonington Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3240, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 9982, "uuid": "7f5c31b4d9f74e81bde883596bb7d79c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/04 over the Sutton Bonington Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 9986, "uuid": "a0631a0e4bd54aa99c3bd304e44f41c7", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/05 over the Western Approaches Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3241, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 9986, "uuid": "a0631a0e4bd54aa99c3bd304e44f41c7", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/05 over the Western Approaches Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3242, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 9986, "uuid": "a0631a0e4bd54aa99c3bd304e44f41c7", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/05 over the Western Approaches Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 9990, "uuid": "60ba84dc8d83429db946fb57a5063aa2", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/06 over the Didcot Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3243, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 9990, "uuid": "60ba84dc8d83429db946fb57a5063aa2", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/06 over the Didcot Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3244, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 9990, "uuid": "60ba84dc8d83429db946fb57a5063aa2", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/06 over the Didcot Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 9994, "uuid": "640663f6a2e84c2ab7b09e637f91bd44", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/08 over the Theale Area, Reading", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3245, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 9994, "uuid": "640663f6a2e84c2ab7b09e637f91bd44", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/08 over the Theale Area, Reading", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3246, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 9994, "uuid": "640663f6a2e84c2ab7b09e637f91bd44", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/08 over the Theale Area, Reading", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 9998, "uuid": "3fb2a3e0a38e40af95a8502e815bec13", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/10 over the Swansea Bay and Bristol Channel Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3247, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 9998, "uuid": "3fb2a3e0a38e40af95a8502e815bec13", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/10 over the Swansea Bay and Bristol Channel Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3248, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 9998, "uuid": "3fb2a3e0a38e40af95a8502e815bec13", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/10 over the Swansea Bay and Bristol Channel Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10002, "uuid": "aa0bce2cf4bb47ba82e3503b33d51bb6", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/11 over the New Forest", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3249, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10002, "uuid": "aa0bce2cf4bb47ba82e3503b33d51bb6", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/11 over the New Forest", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3250, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10002, "uuid": "aa0bce2cf4bb47ba82e3503b33d51bb6", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/11 over the New Forest", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10006, "uuid": "a142478ee1eb41c798e4f2cd9d154d15", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/12 over the Coed-y-Brenin Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3251, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10006, "uuid": "a142478ee1eb41c798e4f2cd9d154d15", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/12 over the Coed-y-Brenin Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3252, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10006, "uuid": "a142478ee1eb41c798e4f2cd9d154d15", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/12 over the Coed-y-Brenin Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10010, "uuid": "af9c10b6d3a645aabd1b91430c72c165", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/13 over the Ballantrae Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3253, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10010, "uuid": "af9c10b6d3a645aabd1b91430c72c165", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/13 over the Ballantrae Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3254, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10010, "uuid": "af9c10b6d3a645aabd1b91430c72c165", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/13 over the Ballantrae Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10014, "uuid": "3afbc0bd3990403c9fc81a01508f001c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/14 over the Snowdonia Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3255, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10014, "uuid": "3afbc0bd3990403c9fc81a01508f001c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/14 over the Snowdonia Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3256, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10014, "uuid": "3afbc0bd3990403c9fc81a01508f001c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/14 over the Snowdonia Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10018, "uuid": "c30381bfb7f6417baa3d49028290f343", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/15 over the Anglesey Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3257, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10018, "uuid": "c30381bfb7f6417baa3d49028290f343", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/15 over the Anglesey Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3258, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. 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The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. 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The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10026, "uuid": "1366e8f7872a48f990e3b7f2c452f89c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/17 over Loch Leven, Loch Tay and Loch Lomond", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3262, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10026, "uuid": "1366e8f7872a48f990e3b7f2c452f89c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/17 over Loch Leven, Loch Tay and Loch Lomond", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10030, "uuid": "6bad5310ef3149408f89b85fbd773ea2", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/21 over the Braunton Burrows Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3263, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10030, "uuid": "6bad5310ef3149408f89b85fbd773ea2", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/21 over the Braunton Burrows Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3264, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10030, "uuid": "6bad5310ef3149408f89b85fbd773ea2", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/21 over the Braunton Burrows Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10034, "uuid": "4149ea26e1b84ab59827bbc50358ab22", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/22 over the Holderness Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3265, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10034, "uuid": "4149ea26e1b84ab59827bbc50358ab22", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/22 over the Holderness Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3266, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10034, "uuid": "4149ea26e1b84ab59827bbc50358ab22", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/22 over the Holderness Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10038, "uuid": "e2131ce607024d70afd0fe1fce74598e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/24 over the Thetford and Chepstow Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3267, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10038, "uuid": "e2131ce607024d70afd0fe1fce74598e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/24 over the Thetford and Chepstow Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3268, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10038, "uuid": "e2131ce607024d70afd0fe1fce74598e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/24 over the Thetford and Chepstow Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10042, "uuid": "9ac221a917274b9facdeacaadba4168b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/25 over the Theobalds Park Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3269, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10042, "uuid": "9ac221a917274b9facdeacaadba4168b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/25 over the Theobalds Park Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3270, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10042, "uuid": "9ac221a917274b9facdeacaadba4168b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/25 over the Theobalds Park Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10046, "uuid": "6551831833014477a47b8217598d3d8e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/27 over the Strumpshaw, Hickling and Acle Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3271, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10046, "uuid": "6551831833014477a47b8217598d3d8e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/27 over the Strumpshaw, Hickling and Acle Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3272, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10046, "uuid": "6551831833014477a47b8217598d3d8e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/27 over the Strumpshaw, Hickling and Acle Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10050, "uuid": "54f6d95888fd49a7a96a159322ee7d4a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/31 over the Rutland Water Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3273, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10050, "uuid": "54f6d95888fd49a7a96a159322ee7d4a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/31 over the Rutland Water Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3274, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. 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The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10054, "uuid": "e9296c93a2ea40b8ac32ab09c540ff79", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/32 over the Durham Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3276, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10054, "uuid": "e9296c93a2ea40b8ac32ab09c540ff79", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/32 over the Durham Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10058, "uuid": "237d8a2b63c54a9581458697c19bac8d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/33 over the Rothamstead Park Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3277, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10058, "uuid": "237d8a2b63c54a9581458697c19bac8d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/33 over the Rothamstead Park Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3278, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10058, "uuid": "237d8a2b63c54a9581458697c19bac8d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/33 over the Rothamstead Park Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10062, "uuid": "c29129fcc07c42a393416ddbd1ff3772", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/36 over the Dyfed Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3279, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10062, "uuid": "c29129fcc07c42a393416ddbd1ff3772", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/36 over the Dyfed Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3280, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10062, "uuid": "c29129fcc07c42a393416ddbd1ff3772", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 84/36 over the Dyfed Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10066, "uuid": "8d70c455e6ea499db787878a3571336d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/02 over the Gedney Hill Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3281, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10066, "uuid": "8d70c455e6ea499db787878a3571336d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/02 over the Gedney Hill Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3282, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10066, "uuid": "8d70c455e6ea499db787878a3571336d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/02 over the Gedney Hill Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10070, "uuid": "e4e80cabf49a4b1ca8ae987704bea9e0", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/13 over the Portsmouth Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3283, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10070, "uuid": "e4e80cabf49a4b1ca8ae987704bea9e0", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/13 over the Portsmouth Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3284, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10070, "uuid": "e4e80cabf49a4b1ca8ae987704bea9e0", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/13 over the Portsmouth Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10074, "uuid": "07a4d437f17248eb88945ded52a31991", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instrument on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/19 over the Dorchester, Poole, Henley and Dartford Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3285, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10074, "uuid": "07a4d437f17248eb88945ded52a31991", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instrument on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/19 over the Dorchester, Poole, Henley and Dartford Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3286, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10074, "uuid": "07a4d437f17248eb88945ded52a31991", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instrument on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/19 over the Dorchester, Poole, Henley and Dartford Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10078, "uuid": "b03a58c0a0654d1884156b3df8314012", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/22 over the North Yorkshire Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3287, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10078, "uuid": "b03a58c0a0654d1884156b3df8314012", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/22 over the North Yorkshire Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3288, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10078, "uuid": "b03a58c0a0654d1884156b3df8314012", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/22 over the North Yorkshire Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10082, "uuid": "eb4d91cecb964f08bb4ed30c37773036", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/34 over the Nottingham Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3289, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10082, "uuid": "eb4d91cecb964f08bb4ed30c37773036", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/34 over the Nottingham Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3290, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10082, "uuid": "eb4d91cecb964f08bb4ed30c37773036", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/34 over the Nottingham Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10086, "uuid": "426fdede91624502a5b0707925c5bb8c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/36 over the Winchester Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3291, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10086, "uuid": "426fdede91624502a5b0707925c5bb8c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/36 over the Winchester Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3292, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10086, "uuid": "426fdede91624502a5b0707925c5bb8c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/36 over the Winchester Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10090, "uuid": "e22b82d414f2454ca1d4f5bc44ec791d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/43 over the Chatteris Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3293, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10090, "uuid": "e22b82d414f2454ca1d4f5bc44ec791d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/43 over the Chatteris Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3294, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10090, "uuid": "e22b82d414f2454ca1d4f5bc44ec791d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/43 over the Chatteris Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10094, "uuid": "f17ecfe9f018461c8585b794be177df6", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/R4 over the Theobalds Park Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3295, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10094, "uuid": "f17ecfe9f018461c8585b794be177df6", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/R4 over the Theobalds Park Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3296, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10094, "uuid": "f17ecfe9f018461c8585b794be177df6", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/R4 over the Theobalds Park Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10098, "uuid": "e1712bbaae9b4889a0f4d1969369cc0f", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/R5 over the Horsey Mere Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 8692, "uuid": "f6f35b2e9a39416c987e8ff7eca15995", "short_code": "mpop", "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3297, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10098, "uuid": "e1712bbaae9b4889a0f4d1969369cc0f", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/R5 over the Horsey Mere Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } }, { "ob_id": 3298, "platform": { "ob_id": 8691, "uuid": "af74710a0e4b400bafdd3669462728a2", "short_code": "plat", "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft", "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10098, "uuid": "e1712bbaae9b4889a0f4d1969369cc0f", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 83/R5 over the Horsey Mere Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; " } } ] }, { "ob_id": 10102, "uuid": "f0655e9c5fea475a8a1876368ac47fa1", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/02 over the Chepstow and Thetford Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 9049, "uuid": "daa5dc2640f64773b91391310e42a3e7", "short_code": "mpop", "title": "Mobile Platform Operation for: Scottish Aviation Twin Pioneer Aircraft", "abstract": "Mobile Platform Operation related to the: Scottish Aviation Twin Pioneer Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3299, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10102, "uuid": "f0655e9c5fea475a8a1876368ac47fa1", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/02 over the Chepstow and Thetford Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } }, { "ob_id": 3300, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10102, "uuid": "f0655e9c5fea475a8a1876368ac47fa1", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/02 over the Chepstow and Thetford Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } } ] }, { "ob_id": 10106, "uuid": "a64ba548fe49405d9b3d5318ce6c0c81", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/25 over the Gower, Tawe Valley and Crai Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 9049, "uuid": "daa5dc2640f64773b91391310e42a3e7", "short_code": "mpop", "title": "Mobile Platform Operation for: Scottish Aviation Twin Pioneer Aircraft", "abstract": "Mobile Platform Operation related to the: Scottish Aviation Twin Pioneer Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3301, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10106, "uuid": "a64ba548fe49405d9b3d5318ce6c0c81", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/25 over the Gower, Tawe Valley and Crai Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } }, { "ob_id": 3302, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10106, "uuid": "a64ba548fe49405d9b3d5318ce6c0c81", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/25 over the Gower, Tawe Valley and Crai Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } } ] }, { "ob_id": 10110, "uuid": "c1e78bbb74a24d37bdd98b0fcc19009e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/26 over the Lathkill Dale Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 9049, "uuid": "daa5dc2640f64773b91391310e42a3e7", "short_code": "mpop", "title": "Mobile Platform Operation for: Scottish Aviation Twin Pioneer Aircraft", "abstract": "Mobile Platform Operation related to the: Scottish Aviation Twin Pioneer Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3303, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10110, "uuid": "c1e78bbb74a24d37bdd98b0fcc19009e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/26 over the Lathkill Dale Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } }, { "ob_id": 3304, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10110, "uuid": "c1e78bbb74a24d37bdd98b0fcc19009e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/26 over the Lathkill Dale Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } } ] }, { "ob_id": 10114, "uuid": "a481e78774564d19892a9e86ee29a14f", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/34 over the Wymondham Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 9049, "uuid": "daa5dc2640f64773b91391310e42a3e7", "short_code": "mpop", "title": "Mobile Platform Operation for: Scottish Aviation Twin Pioneer Aircraft", "abstract": "Mobile Platform Operation related to the: Scottish Aviation Twin Pioneer Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3305, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10114, "uuid": "a481e78774564d19892a9e86ee29a14f", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/34 over the Wymondham Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } }, { "ob_id": 3306, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10114, "uuid": "a481e78774564d19892a9e86ee29a14f", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/34 over the Wymondham Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } } ] }, { "ob_id": 10118, "uuid": "98d071b023764e35868eb3105aaa78de", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/39 over The Severn Estuary and The Wash", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 9049, "uuid": "daa5dc2640f64773b91391310e42a3e7", "short_code": "mpop", "title": "Mobile Platform Operation for: Scottish Aviation Twin Pioneer Aircraft", "abstract": "Mobile Platform Operation related to the: Scottish Aviation Twin Pioneer Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3307, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10118, "uuid": "98d071b023764e35868eb3105aaa78de", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/39 over The Severn Estuary and The Wash", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } }, { "ob_id": 3308, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10118, "uuid": "98d071b023764e35868eb3105aaa78de", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/39 over The Severn Estuary and The Wash", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } } ] }, { "ob_id": 10122, "uuid": "5918ee113f8548ad8b0f5b363d5e7da6", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/40 over the Norton Lindsey Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 9049, "uuid": "daa5dc2640f64773b91391310e42a3e7", "short_code": "mpop", "title": "Mobile Platform Operation for: Scottish Aviation Twin Pioneer Aircraft", "abstract": "Mobile Platform Operation related to the: Scottish Aviation Twin Pioneer Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3309, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10122, "uuid": "5918ee113f8548ad8b0f5b363d5e7da6", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/40 over the Norton Lindsey Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } }, { "ob_id": 3310, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10122, "uuid": "5918ee113f8548ad8b0f5b363d5e7da6", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/40 over the Norton Lindsey Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } } ] }, { "ob_id": 10126, "uuid": "43b416d04caf49a48be35e4829bc81fe", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/41 over the Shapwick, Gedney Hill, Chatteris and Strumpshaw Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 9049, "uuid": "daa5dc2640f64773b91391310e42a3e7", "short_code": "mpop", "title": "Mobile Platform Operation for: Scottish Aviation Twin Pioneer Aircraft", "abstract": "Mobile Platform Operation related to the: Scottish Aviation Twin Pioneer Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3311, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10126, "uuid": "43b416d04caf49a48be35e4829bc81fe", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/41 over the Shapwick, Gedney Hill, Chatteris and Strumpshaw Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } }, { "ob_id": 3312, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10126, "uuid": "43b416d04caf49a48be35e4829bc81fe", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/41 over the Shapwick, Gedney Hill, Chatteris and Strumpshaw Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } } ] }, { "ob_id": 10130, "uuid": "4123dc9ea04c4e2297351a5c8b3c7de5", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/43 over the Broads Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 9049, "uuid": "daa5dc2640f64773b91391310e42a3e7", "short_code": "mpop", "title": "Mobile Platform Operation for: Scottish Aviation Twin Pioneer Aircraft", "abstract": "Mobile Platform Operation related to the: Scottish Aviation Twin Pioneer Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3313, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10130, "uuid": "4123dc9ea04c4e2297351a5c8b3c7de5", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/43 over the Broads Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } }, { "ob_id": 3314, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10130, "uuid": "4123dc9ea04c4e2297351a5c8b3c7de5", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/43 over the Broads Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } } ] }, { "ob_id": 10134, "uuid": "b7a06cfb18cd4dfb9a48d959ff977987", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/test over the Conington Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 9049, "uuid": "daa5dc2640f64773b91391310e42a3e7", "short_code": "mpop", "title": "Mobile Platform Operation for: Scottish Aviation Twin Pioneer Aircraft", "abstract": "Mobile Platform Operation related to the: Scottish Aviation Twin Pioneer Aircraft" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3315, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8855, "uuid": "675df2bd79404c8ba30c6991111df9e7", "short_code": "instr", "title": "ARSF WILD-RC8 Analogue Photographic camera", "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n" }, "relatedTo": { "ob_id": 10134, "uuid": "b7a06cfb18cd4dfb9a48d959ff977987", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/test over the Conington Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } }, { "ob_id": 3316, "platform": { "ob_id": 9048, "uuid": "abf8b3c78fe74486a730180d12526196", "short_code": "plat", "title": "Scottish Aviation Twin Pioneer Aircraft", "abstract": "A Scottish Aviation Twin Pioneer Aircraft, registration G-AZHJ, used for the Airborne Research and Survey Facility (ARSF) survey flights in 1982." }, "instrument": { "ob_id": 8754, "uuid": "967ae4b17bf145d8a8a6982a648d64d5", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268", "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998." }, "relatedTo": { "ob_id": 10134, "uuid": "b7a06cfb18cd4dfb9a48d959ff977987", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Scottish Aviation Twin Pioneer Aircraft during Flight 82/test over the Conington Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Scottish Aviation Twin Pioneer Aircraft; " } } ] }, { "ob_id": 10138, "uuid": "1a64f5299b8c4a0b8eb507be18df2108", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/33 over Mount Etna Volcano, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3317, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10138, "uuid": "1a64f5299b8c4a0b8eb507be18df2108", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/33 over Mount Etna Volcano, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3318, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10138, "uuid": "1a64f5299b8c4a0b8eb507be18df2108", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/33 over Mount Etna Volcano, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10142, "uuid": "0c5d46934c704b04aee646947abe4267", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/32 over the Latera Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3319, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10142, "uuid": "0c5d46934c704b04aee646947abe4267", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/32 over the Latera Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3320, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10142, "uuid": "0c5d46934c704b04aee646947abe4267", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/32 over the Latera Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3321, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10142, "uuid": "0c5d46934c704b04aee646947abe4267", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/32 over the Latera Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10146, "uuid": "d5e508ffdb854cbebe7b83c04ccf871e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/31 over the Paphos Area, Cyprus", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3322, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10146, "uuid": "d5e508ffdb854cbebe7b83c04ccf871e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/31 over the Paphos Area, Cyprus", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3323, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10146, "uuid": "d5e508ffdb854cbebe7b83c04ccf871e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/31 over the Paphos Area, Cyprus", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10150, "uuid": "6c40ab4a13d141a4829c4bcc1e86ff7e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/30 over the Troodos Area, Cyprus", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3324, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10150, "uuid": "6c40ab4a13d141a4829c4bcc1e86ff7e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/30 over the Troodos Area, Cyprus", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3325, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10150, "uuid": "6c40ab4a13d141a4829c4bcc1e86ff7e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/30 over the Troodos Area, Cyprus", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3326, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10150, "uuid": "6c40ab4a13d141a4829c4bcc1e86ff7e", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/30 over the Troodos Area, Cyprus", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10154, "uuid": "52f9f8a5571146178c08346b70a6b1c5", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/29 over the Venice Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3327, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10154, "uuid": "52f9f8a5571146178c08346b70a6b1c5", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/29 over the Venice Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3328, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10154, "uuid": "52f9f8a5571146178c08346b70a6b1c5", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/29 over the Venice Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3329, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10154, "uuid": "52f9f8a5571146178c08346b70a6b1c5", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/29 over the Venice Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10158, "uuid": "7e1e9f80555b491a8084ba551a851897", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/28 over the Castelvetrano and Maganoce Areas, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3330, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10158, "uuid": "7e1e9f80555b491a8084ba551a851897", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/28 over the Castelvetrano and Maganoce Areas, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3331, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10158, "uuid": "7e1e9f80555b491a8084ba551a851897", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/28 over the Castelvetrano and Maganoce Areas, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3332, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10158, "uuid": "7e1e9f80555b491a8084ba551a851897", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/28 over the Castelvetrano and Maganoce Areas, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10162, "uuid": "5035f1e436c044909c9295527d13bb0b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/24 over the Nepi Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3333, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10162, "uuid": "5035f1e436c044909c9295527d13bb0b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/24 over the Nepi Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3334, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10162, "uuid": "5035f1e436c044909c9295527d13bb0b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/24 over the Nepi Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3335, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10162, "uuid": "5035f1e436c044909c9295527d13bb0b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/24 over the Nepi Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3336, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10162, "uuid": "5035f1e436c044909c9295527d13bb0b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/24 over the Nepi Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10166, "uuid": "6c15ebac3ba54c3399887d18aaf8f91b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/20 over the Spilimbergo Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3337, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10166, "uuid": "6c15ebac3ba54c3399887d18aaf8f91b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/20 over the Spilimbergo Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3338, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10166, "uuid": "6c15ebac3ba54c3399887d18aaf8f91b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/20 over the Spilimbergo Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3339, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10166, "uuid": "6c15ebac3ba54c3399887d18aaf8f91b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/20 over the Spilimbergo Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10170, "uuid": "0063e2107a914359a2391c171ea8050a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/16 over the Khora Sfakion Area, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3340, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10170, "uuid": "0063e2107a914359a2391c171ea8050a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/16 over the Khora Sfakion Area, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3341, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10170, "uuid": "0063e2107a914359a2391c171ea8050a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/16 over the Khora Sfakion Area, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3342, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10170, "uuid": "0063e2107a914359a2391c171ea8050a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/16 over the Khora Sfakion Area, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10174, "uuid": "68e8ada6087f41a1bd2b0005d36f847b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/15 over the Sitia Area, Crete", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3343, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10174, "uuid": "68e8ada6087f41a1bd2b0005d36f847b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/15 over the Sitia Area, Crete", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3344, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10174, "uuid": "68e8ada6087f41a1bd2b0005d36f847b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/15 over the Sitia Area, Crete", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3345, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10174, "uuid": "68e8ada6087f41a1bd2b0005d36f847b", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/15 over the Sitia Area, Crete", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10178, "uuid": "e476d1e1c3894137a66ba2b99849c225", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/14 over the Cersosimo and Arpi Areas, Italy, and the Heslerton Area, UK", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3346, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10178, "uuid": "e476d1e1c3894137a66ba2b99849c225", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/14 over the Cersosimo and Arpi Areas, Italy, and the Heslerton Area, UK", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3347, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10178, "uuid": "e476d1e1c3894137a66ba2b99849c225", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/14 over the Cersosimo and Arpi Areas, Italy, and the Heslerton Area, UK", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3348, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10178, "uuid": "e476d1e1c3894137a66ba2b99849c225", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/14 over the Cersosimo and Arpi Areas, Italy, and the Heslerton Area, UK", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3349, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10178, "uuid": "e476d1e1c3894137a66ba2b99849c225", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/14 over the Cersosimo and Arpi Areas, Italy, and the Heslerton Area, UK", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10182, "uuid": "468b50c9263b47a5b598466d9e421b10", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/10 over Milos Island, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3350, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10182, "uuid": "468b50c9263b47a5b598466d9e421b10", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/10 over Milos Island, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3351, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10182, "uuid": "468b50c9263b47a5b598466d9e421b10", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/10 over Milos Island, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3352, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10182, "uuid": "468b50c9263b47a5b598466d9e421b10", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/10 over Milos Island, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3353, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10182, "uuid": "468b50c9263b47a5b598466d9e421b10", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/10 over Milos Island, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10186, "uuid": "38376701155d4228866e60f9ed5026ae", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/07 over the Pollino, Tuscania and Tarquinia Areas, Spain", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3354, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10186, "uuid": "38376701155d4228866e60f9ed5026ae", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/07 over the Pollino, Tuscania and Tarquinia Areas, Spain", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3355, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10186, "uuid": "38376701155d4228866e60f9ed5026ae", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/07 over the Pollino, Tuscania and Tarquinia Areas, Spain", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3356, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10186, "uuid": "38376701155d4228866e60f9ed5026ae", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/07 over the Pollino, Tuscania and Tarquinia Areas, Spain", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3357, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10186, "uuid": "38376701155d4228866e60f9ed5026ae", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/07 over the Pollino, Tuscania and Tarquinia Areas, Spain", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10190, "uuid": "835a83788403458c8d3e816d1b3b4916", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2005/14 over the North York Moors Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3358, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10190, "uuid": "835a83788403458c8d3e816d1b3b4916", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2005/14 over the North York Moors Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3359, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10190, "uuid": "835a83788403458c8d3e816d1b3b4916", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2005/14 over the North York Moors Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10194, "uuid": "3592b7fae1db4f66834bc45c2004b904", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2005/13 over the Plymouth Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3360, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10194, "uuid": "3592b7fae1db4f66834bc45c2004b904", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2005/13 over the Plymouth Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3361, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10194, "uuid": "3592b7fae1db4f66834bc45c2004b904", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2005/13 over the Plymouth Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3362, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10194, "uuid": "3592b7fae1db4f66834bc45c2004b904", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2005/13 over the Plymouth Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10198, "uuid": "5ec90aab69694d7c9902f0f786f1d66d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2004/23 over the Filey Bay, Robin Hood's Bay and Whitby Abbey Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3363, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10198, "uuid": "5ec90aab69694d7c9902f0f786f1d66d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2004/23 over the Filey Bay, Robin Hood's Bay and Whitby Abbey Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3364, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10198, "uuid": "5ec90aab69694d7c9902f0f786f1d66d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2004/23 over the Filey Bay, Robin Hood's Bay and Whitby Abbey Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3365, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10198, "uuid": "5ec90aab69694d7c9902f0f786f1d66d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2004/23 over the Filey Bay, Robin Hood's Bay and Whitby Abbey Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3366, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10198, "uuid": "5ec90aab69694d7c9902f0f786f1d66d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2004/23 over the Filey Bay, Robin Hood's Bay and Whitby Abbey Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10203, "uuid": "c3594265a49f4ed09707b96e293274fb", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight GB05/02 over the Dee Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Rollei Digital Camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3367, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10203, "uuid": "c3594265a49f4ed09707b96e293274fb", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight GB05/02 over the Dee Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Rollei Digital Camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3368, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 10202, "uuid": "4ba81218ece24bb89ed01d615e39be05", "short_code": "instr", "title": "ARSF Rollei Digital Camera", "abstract": "The ARSF ROLLEI digital camera is used to obtain imagery at the same time as the other instruments. This camera replaces the previous film format Wild RC series cameras(?)" }, "relatedTo": { "ob_id": 10203, "uuid": "c3594265a49f4ed09707b96e293274fb", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight GB05/02 over the Dee Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Rollei Digital Camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3369, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10203, "uuid": "c3594265a49f4ed09707b96e293274fb", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight GB05/02 over the Dee Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Rollei Digital Camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3370, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10203, "uuid": "c3594265a49f4ed09707b96e293274fb", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight GB05/02 over the Dee Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Rollei Digital Camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10207, "uuid": "e2153c7da4d74f069be0ceaf9cf01d57", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight GB05/01 over the Edinburgh and Glasgow Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Rollei Digital Camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3371, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10207, "uuid": "e2153c7da4d74f069be0ceaf9cf01d57", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight GB05/01 over the Edinburgh and Glasgow Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Rollei Digital Camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3372, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10207, "uuid": "e2153c7da4d74f069be0ceaf9cf01d57", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight GB05/01 over the Edinburgh and Glasgow Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Rollei Digital Camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3373, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 10202, "uuid": "4ba81218ece24bb89ed01d615e39be05", "short_code": "instr", "title": "ARSF Rollei Digital Camera", "abstract": "The ARSF ROLLEI digital camera is used to obtain imagery at the same time as the other instruments. This camera replaces the previous film format Wild RC series cameras(?)" }, "relatedTo": { "ob_id": 10207, "uuid": "e2153c7da4d74f069be0ceaf9cf01d57", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight GB05/01 over the Edinburgh and Glasgow Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Rollei Digital Camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3374, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10207, "uuid": "e2153c7da4d74f069be0ceaf9cf01d57", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight GB05/01 over the Edinburgh and Glasgow Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Rollei Digital Camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10211, "uuid": "cb65d203f79442b6aca6827977cb5f68", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Calibration Flight 05/cal over the Monks Wood Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3375, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10211, "uuid": "cb65d203f79442b6aca6827977cb5f68", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Calibration Flight 05/cal over the Monks Wood Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3376, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10211, "uuid": "cb65d203f79442b6aca6827977cb5f68", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Calibration Flight 05/cal over the Monks Wood Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10215, "uuid": "38466e9dc6ef42ae90a366018be67fca", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB03/13 over the Wytham Woods Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3377, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10215, "uuid": "38466e9dc6ef42ae90a366018be67fca", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB03/13 over the Wytham Woods Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3378, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10215, "uuid": "38466e9dc6ef42ae90a366018be67fca", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB03/13 over the Wytham Woods Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10219, "uuid": "2576e243938a4fde804119d6945bb070", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/29 over the Glen Ogle and Glen Ample Landslides and Deposits", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3379, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10219, "uuid": "2576e243938a4fde804119d6945bb070", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/29 over the Glen Ogle and Glen Ample Landslides and Deposits", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3380, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10219, "uuid": "2576e243938a4fde804119d6945bb070", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/29 over the Glen Ogle and Glen Ample Landslides and Deposits", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3381, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10219, "uuid": "2576e243938a4fde804119d6945bb070", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/29 over the Glen Ogle and Glen Ample Landslides and Deposits", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10223, "uuid": "f79b726e80994216aa252936fe4248e7", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight 04/16 over the Norfolk Broads Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Rollei Digital Camera, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3382, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10223, "uuid": "f79b726e80994216aa252936fe4248e7", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight 04/16 over the Norfolk Broads Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Rollei Digital Camera, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3383, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10223, "uuid": "f79b726e80994216aa252936fe4248e7", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight 04/16 over the Norfolk Broads Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Rollei Digital Camera, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3384, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 10202, "uuid": "4ba81218ece24bb89ed01d615e39be05", "short_code": "instr", "title": "ARSF Rollei Digital Camera", "abstract": "The ARSF ROLLEI digital camera is used to obtain imagery at the same time as the other instruments. This camera replaces the previous film format Wild RC series cameras(?)" }, "relatedTo": { "ob_id": 10223, "uuid": "f79b726e80994216aa252936fe4248e7", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight 04/16 over the Norfolk Broads Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Rollei Digital Camera, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3385, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10223, "uuid": "f79b726e80994216aa252936fe4248e7", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight 04/16 over the Norfolk Broads Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Rollei Digital Camera, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10227, "uuid": "366740615bbd44a29cda0a2515052220", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/03 over the Sheffield, Cardiff and Cambridge Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3386, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10227, "uuid": "366740615bbd44a29cda0a2515052220", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/03 over the Sheffield, Cardiff and Cambridge Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3387, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10227, "uuid": "366740615bbd44a29cda0a2515052220", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/03 over the Sheffield, Cardiff and Cambridge Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3388, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10227, "uuid": "366740615bbd44a29cda0a2515052220", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/03 over the Sheffield, Cardiff and Cambridge Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10231, "uuid": "16370d72b983417eadddbc12e2a6e15c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/02 over the Conwy Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3389, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10231, "uuid": "16370d72b983417eadddbc12e2a6e15c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/02 over the Conwy Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3390, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10231, "uuid": "16370d72b983417eadddbc12e2a6e15c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/02 over the Conwy Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3391, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10231, "uuid": "16370d72b983417eadddbc12e2a6e15c", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/02 over the Conwy Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10235, "uuid": "1327b571d786496cb2269ada17b34f2d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/16 over the Gulfaske, Albrecht, Slakbreen, Bakaninbreen, Midrelovenbreen, Austrbrogger, Finsterwalderbreen, Fridtjonbreen and Koristka Areas, Svalbard, for the Norwegian Polar Institute", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3392, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10235, "uuid": "1327b571d786496cb2269ada17b34f2d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/16 over the Gulfaske, Albrecht, Slakbreen, Bakaninbreen, Midrelovenbreen, Austrbrogger, Finsterwalderbreen, Fridtjonbreen and Koristka Areas, Svalbard, for the Norwegian Polar Institute", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3393, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10235, "uuid": "1327b571d786496cb2269ada17b34f2d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/16 over the Gulfaske, Albrecht, Slakbreen, Bakaninbreen, Midrelovenbreen, Austrbrogger, Finsterwalderbreen, Fridtjonbreen and Koristka Areas, Svalbard, for the Norwegian Polar Institute", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3394, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10235, "uuid": "1327b571d786496cb2269ada17b34f2d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/16 over the Gulfaske, Albrecht, Slakbreen, Bakaninbreen, Midrelovenbreen, Austrbrogger, Finsterwalderbreen, Fridtjonbreen and Koristka Areas, Svalbard, for the Norwegian Polar Institute", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10239, "uuid": "a965f0daa6cf43188a6525c2cfd1f551", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/15 over the Wytham Woods Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3395, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10239, "uuid": "a965f0daa6cf43188a6525c2cfd1f551", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/15 over the Wytham Woods Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3396, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10239, "uuid": "a965f0daa6cf43188a6525c2cfd1f551", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/15 over the Wytham Woods Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10243, "uuid": "52879e6d1ad54692b2454c00c1242041", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/04 over the Midrelovenbreen Area, Svalbard, for the Norwegian Polar Institute", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3397, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10243, "uuid": "52879e6d1ad54692b2454c00c1242041", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/04 over the Midrelovenbreen Area, Svalbard, for the Norwegian Polar Institute", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3398, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10243, "uuid": "52879e6d1ad54692b2454c00c1242041", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/04 over the Midrelovenbreen Area, Svalbard, for the Norwegian Polar Institute", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3399, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10243, "uuid": "52879e6d1ad54692b2454c00c1242041", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/04 over the Midrelovenbreen Area, Svalbard, for the Norwegian Polar Institute", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3400, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10243, "uuid": "52879e6d1ad54692b2454c00c1242041", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/04 over the Midrelovenbreen Area, Svalbard, for the Norwegian Polar Institute", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10247, "uuid": "efbf093eb10b45a0bc111339b6e8e21d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/19 over the Monks Wood and Woodwalton Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3401, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10247, "uuid": "efbf093eb10b45a0bc111339b6e8e21d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/19 over the Monks Wood and Woodwalton Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3402, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10247, "uuid": "efbf093eb10b45a0bc111339b6e8e21d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/19 over the Monks Wood and Woodwalton Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3403, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10247, "uuid": "efbf093eb10b45a0bc111339b6e8e21d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/19 over the Monks Wood and Woodwalton Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10251, "uuid": "b839d885ee054a0ba26127bbee73818e", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight 01/12 over the Llangattock and Ripon Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Rollei Digital Camera; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3404, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10251, "uuid": "b839d885ee054a0ba26127bbee73818e", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight 01/12 over the Llangattock and Ripon Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Rollei Digital Camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3405, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10251, "uuid": "b839d885ee054a0ba26127bbee73818e", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight 01/12 over the Llangattock and Ripon Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Rollei Digital Camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3406, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10251, "uuid": "b839d885ee054a0ba26127bbee73818e", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight 01/12 over the Llangattock and Ripon Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Rollei Digital Camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3407, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 10202, "uuid": "4ba81218ece24bb89ed01d615e39be05", "short_code": "instr", "title": "ARSF Rollei Digital Camera", "abstract": "The ARSF ROLLEI digital camera is used to obtain imagery at the same time as the other instruments. This camera replaces the previous film format Wild RC series cameras(?)" }, "relatedTo": { "ob_id": 10251, "uuid": "b839d885ee054a0ba26127bbee73818e", "short_code": "acq", "title": "Acquisition Process for: Data from the Rollei Digital Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during flight 01/12 over the Llangattock and Ripon Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Rollei Digital Camera; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10255, "uuid": "a03251ccf7a14d1c83731bdd8a98d833", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/17 over the Abisko Area, Sweden", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3408, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10255, "uuid": "a03251ccf7a14d1c83731bdd8a98d833", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/17 over the Abisko Area, Sweden", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3409, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10255, "uuid": "a03251ccf7a14d1c83731bdd8a98d833", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/17 over the Abisko Area, Sweden", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3410, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10255, "uuid": "a03251ccf7a14d1c83731bdd8a98d833", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/17 over the Abisko Area, Sweden", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3411, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10255, "uuid": "a03251ccf7a14d1c83731bdd8a98d833", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/17 over the Abisko Area, Sweden", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10259, "uuid": "fdd2432715d747ceb9a3bee18efe7d7e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/16 over the Tamar Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3412, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10259, "uuid": "fdd2432715d747ceb9a3bee18efe7d7e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/16 over the Tamar Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3413, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10259, "uuid": "fdd2432715d747ceb9a3bee18efe7d7e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/16 over the Tamar Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10263, "uuid": "221dff0e2a9a429ea2d7a539c5b04207", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/10 over the Lakselv and Divadalen Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3414, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10263, "uuid": "221dff0e2a9a429ea2d7a539c5b04207", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/10 over the Lakselv and Divadalen Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3415, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10263, "uuid": "221dff0e2a9a429ea2d7a539c5b04207", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/10 over the Lakselv and Divadalen Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3416, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10263, "uuid": "221dff0e2a9a429ea2d7a539c5b04207", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/10 over the Lakselv and Divadalen Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10267, "uuid": "48b5a98211254b5ea5e4cf29b95eedb2", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/11 over the Sheep House Wood, Wytham Wood and Brampton Wood Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3417, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10267, "uuid": "48b5a98211254b5ea5e4cf29b95eedb2", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/11 over the Sheep House Wood, Wytham Wood and Brampton Wood Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3418, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10267, "uuid": "48b5a98211254b5ea5e4cf29b95eedb2", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/11 over the Sheep House Wood, Wytham Wood and Brampton Wood Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3419, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10267, "uuid": "48b5a98211254b5ea5e4cf29b95eedb2", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/11 over the Sheep House Wood, Wytham Wood and Brampton Wood Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10271, "uuid": "a19d074162ff48428613495a51e7563e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/05 over the Harwood Forest Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3420, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10271, "uuid": "a19d074162ff48428613495a51e7563e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/05 over the Harwood Forest Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3421, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10271, "uuid": "a19d074162ff48428613495a51e7563e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/05 over the Harwood Forest Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10275, "uuid": "037419e033bc41219a0af56a12d87b8e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/09 over the Wantage Area, in support of the LOwland CAtchment Research programme (LOCAR)", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3422, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10275, "uuid": "037419e033bc41219a0af56a12d87b8e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/09 over the Wantage Area, in support of the LOwland CAtchment Research programme (LOCAR)", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3423, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10275, "uuid": "037419e033bc41219a0af56a12d87b8e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/09 over the Wantage Area, in support of the LOwland CAtchment Research programme (LOCAR)", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10279, "uuid": "959fe172f87f4a819ca4c470e3c2b403", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/11 over the Plymouth Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3424, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10279, "uuid": "959fe172f87f4a819ca4c470e3c2b403", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/11 over the Plymouth Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3425, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10279, "uuid": "959fe172f87f4a819ca4c470e3c2b403", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/11 over the Plymouth Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3426, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10279, "uuid": "959fe172f87f4a819ca4c470e3c2b403", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/11 over the Plymouth Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10283, "uuid": "268516c59e364d56bc77d2ee625e0984", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/13 over The Irish Sea", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3427, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10283, "uuid": "268516c59e364d56bc77d2ee625e0984", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/13 over The Irish Sea", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3428, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10283, "uuid": "268516c59e364d56bc77d2ee625e0984", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/13 over The Irish Sea", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10287, "uuid": "abffbc928bec468b8a394d20f9ec7f7a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/17 over the Manchester Area, in support of the Adaption Strategies to Climate Change in the Urban Environment (ASCCUE) Project", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3429, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10287, "uuid": "abffbc928bec468b8a394d20f9ec7f7a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/17 over the Manchester Area, in support of the Adaption Strategies to Climate Change in the Urban Environment (ASCCUE) Project", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3430, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10287, "uuid": "abffbc928bec468b8a394d20f9ec7f7a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/17 over the Manchester Area, in support of the Adaption Strategies to Climate Change in the Urban Environment (ASCCUE) Project", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10291, "uuid": "9bb92113722e4abcbe018745a31cd425", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/18 over the Insh Marshes Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3431, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10291, "uuid": "9bb92113722e4abcbe018745a31cd425", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/18 over the Insh Marshes Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3432, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10291, "uuid": "9bb92113722e4abcbe018745a31cd425", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/18 over the Insh Marshes Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10295, "uuid": "c2dcdd81b4414e52b5d82ae66f4c3685", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/19 over the Nigg Bay Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3433, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10295, "uuid": "c2dcdd81b4414e52b5d82ae66f4c3685", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/19 over the Nigg Bay Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3434, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10295, "uuid": "c2dcdd81b4414e52b5d82ae66f4c3685", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/19 over the Nigg Bay Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10299, "uuid": "80f15d0bdc7e410490bdd0a911c98f30", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/26 over the Pipeline through Aberdeenshire", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3435, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10299, "uuid": "80f15d0bdc7e410490bdd0a911c98f30", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/26 over the Pipeline through Aberdeenshire", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3436, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10299, "uuid": "80f15d0bdc7e410490bdd0a911c98f30", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/26 over the Pipeline through Aberdeenshire", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10303, "uuid": "7414a167ebea409290a09ec082e015c9", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/28 over the Northborough Area, for Time Team", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3437, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10303, "uuid": "7414a167ebea409290a09ec082e015c9", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/28 over the Northborough Area, for Time Team", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3438, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10303, "uuid": "7414a167ebea409290a09ec082e015c9", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 04/28 over the Northborough Area, for Time Team", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10307, "uuid": "a051d090b66444cd8d104d7268cab00e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/03/12 over the Spilli, Mires, Plakiotissa and Zaros Areas, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3439, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10307, "uuid": "a051d090b66444cd8d104d7268cab00e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/03/12 over the Spilli, Mires, Plakiotissa and Zaros Areas, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3440, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10307, "uuid": "a051d090b66444cd8d104d7268cab00e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/03/12 over the Spilli, Mires, Plakiotissa and Zaros Areas, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10311, "uuid": "9d30fe7a0f67444b90780d2ad57e6920", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/12 over the Spilli, Mires, Plakiotissa and Zaros Areas, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3441, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10311, "uuid": "9d30fe7a0f67444b90780d2ad57e6920", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/12 over the Spilli, Mires, Plakiotissa and Zaros Areas, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3442, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10311, "uuid": "9d30fe7a0f67444b90780d2ad57e6920", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/12 over the Spilli, Mires, Plakiotissa and Zaros Areas, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3443, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10311, "uuid": "9d30fe7a0f67444b90780d2ad57e6920", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/12 over the Spilli, Mires, Plakiotissa and Zaros Areas, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10315, "uuid": "cb2a0e91c2314090943475cfc6a2ebe4", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/19 over the Collazzone Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3444, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10315, "uuid": "cb2a0e91c2314090943475cfc6a2ebe4", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/19 over the Collazzone Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3445, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10315, "uuid": "cb2a0e91c2314090943475cfc6a2ebe4", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/19 over the Collazzone Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3446, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10315, "uuid": "cb2a0e91c2314090943475cfc6a2ebe4", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/19 over the Collazzone Area, Italy", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10319, "uuid": "afae4783ae934ab1aff4ed53794f0c4a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/21 over the Kameni and Santorini Islands, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3447, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10319, "uuid": "afae4783ae934ab1aff4ed53794f0c4a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/21 over the Kameni and Santorini Islands, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3448, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10319, "uuid": "afae4783ae934ab1aff4ed53794f0c4a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/21 over the Kameni and Santorini Islands, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3449, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10319, "uuid": "afae4783ae934ab1aff4ed53794f0c4a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/21 over the Kameni and Santorini Islands, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3450, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10319, "uuid": "afae4783ae934ab1aff4ed53794f0c4a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/21 over the Kameni and Santorini Islands, Greece", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10323, "uuid": "f3487e611200466ab68dfd00c02304bf", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/22 over the Palekastro and Itanos Areas, Crete", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3451, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10323, "uuid": "f3487e611200466ab68dfd00c02304bf", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/22 over the Palekastro and Itanos Areas, Crete", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3452, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8621, "uuid": "29e351cfcf014044af5f9f1e3d3678d0", "short_code": "instr", "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR", "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University" }, "relatedTo": { "ob_id": 10323, "uuid": "f3487e611200466ab68dfd00c02304bf", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/22 over the Palekastro and Itanos Areas, Crete", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3453, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10323, "uuid": "f3487e611200466ab68dfd00c02304bf", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/22 over the Palekastro and Itanos Areas, Crete", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3454, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10323, "uuid": "f3487e611200466ab68dfd00c02304bf", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/22 over the Palekastro and Itanos Areas, Crete", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10327, "uuid": "5576639cae1e4d3890f1129eff89ae31", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 00/02 over the Insh Marshes Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3455, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10327, "uuid": "5576639cae1e4d3890f1129eff89ae31", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 00/02 over the Insh Marshes Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3456, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10327, "uuid": "5576639cae1e4d3890f1129eff89ae31", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 00/02 over the Insh Marshes Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10331, "uuid": "120a092ef10b4dd5a42a27e1e6ad2d82", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/03 over the Ribble Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3457, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10331, "uuid": "120a092ef10b4dd5a42a27e1e6ad2d82", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/03 over the Ribble Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3458, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10331, "uuid": "120a092ef10b4dd5a42a27e1e6ad2d82", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/03 over the Ribble Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3459, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10331, "uuid": "120a092ef10b4dd5a42a27e1e6ad2d82", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/03 over the Ribble Estuary", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10335, "uuid": "019ac9d118c842e695f0dc8e0812ea41", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/26 over the Woodwalton Fen, Woodwalton and Monks Wood Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3460, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10335, "uuid": "019ac9d118c842e695f0dc8e0812ea41", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/26 over the Woodwalton Fen, Woodwalton and Monks Wood Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3461, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10335, "uuid": "019ac9d118c842e695f0dc8e0812ea41", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/26 over the Woodwalton Fen, Woodwalton and Monks Wood Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3462, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10335, "uuid": "019ac9d118c842e695f0dc8e0812ea41", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/26 over the Woodwalton Fen, Woodwalton and Monks Wood Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10339, "uuid": "34854caf58694e1f827d994f4cd577a2", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/03 over the Llangattock Plateau Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3463, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10339, "uuid": "34854caf58694e1f827d994f4cd577a2", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/03 over the Llangattock Plateau Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3464, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10339, "uuid": "34854caf58694e1f827d994f4cd577a2", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/03 over the Llangattock Plateau Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10343, "uuid": "e6abea400a704dafb0c177783e3255aa", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/09 over the Houghton le Spring and New Biggin Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3465, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10343, "uuid": "e6abea400a704dafb0c177783e3255aa", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/09 over the Houghton le Spring and New Biggin Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3466, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10343, "uuid": "e6abea400a704dafb0c177783e3255aa", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/09 over the Houghton le Spring and New Biggin Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3467, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10343, "uuid": "e6abea400a704dafb0c177783e3255aa", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/09 over the Houghton le Spring and New Biggin Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10347, "uuid": "ac337948eef64c46a40a174194905dd5", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/18 over the Calstock and Plymouth Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3468, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10347, "uuid": "ac337948eef64c46a40a174194905dd5", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/18 over the Calstock and Plymouth Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3469, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10347, "uuid": "ac337948eef64c46a40a174194905dd5", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/18 over the Calstock and Plymouth Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3470, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10347, "uuid": "ac337948eef64c46a40a174194905dd5", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/18 over the Calstock and Plymouth Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10351, "uuid": "0149f967daf44f1d810b0a660b127e69", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/31 over the Kelso Area, for Time Team", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3471, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10351, "uuid": "0149f967daf44f1d810b0a660b127e69", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/31 over the Kelso Area, for Time Team", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3472, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10351, "uuid": "0149f967daf44f1d810b0a660b127e69", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/31 over the Kelso Area, for Time Team", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3473, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10351, "uuid": "0149f967daf44f1d810b0a660b127e69", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/31 over the Kelso Area, for Time Team", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10355, "uuid": "afed1e79d1e840d9b929a25598647f8d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 00/03 over the Blackbrook Catchment Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3474, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10355, "uuid": "afed1e79d1e840d9b929a25598647f8d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 00/03 over the Blackbrook Catchment Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3475, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10355, "uuid": "afed1e79d1e840d9b929a25598647f8d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 00/03 over the Blackbrook Catchment Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3476, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10355, "uuid": "afed1e79d1e840d9b929a25598647f8d", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 00/03 over the Blackbrook Catchment Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10359, "uuid": "ee84934255bc49d2a69526880a5d1a3a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 00/16 over the Salisbury Plain Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3477, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8608, "uuid": "b253208e4d394fb5803379bd0f39dec7", "short_code": "instr", "title": "ARSF WILD-RC10 Analogue Photographic camera", "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format." }, "relatedTo": { "ob_id": 10359, "uuid": "ee84934255bc49d2a69526880a5d1a3a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 00/16 over the Salisbury Plain Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3478, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10359, "uuid": "ee84934255bc49d2a69526880a5d1a3a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 00/16 over the Salisbury Plain Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3479, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10359, "uuid": "ee84934255bc49d2a69526880a5d1a3a", "short_code": "acq", "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 00/16 over the Salisbury Plain Area", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] }, { "ob_id": 10363, "uuid": "f5ca7b5b2e4f45b08b85f557cfe1528e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain Aircraft during Flight 00/24 over the Nottingham and Chesterfield Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; ", "imageDetails": [], "mobilePlatformOperation": [ { "ob_id": 6410, "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671", "short_code": "mpop", "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM", "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM" } ], "independentInstrument": [], "instrumentplatformpair_set": [ { "ob_id": 3480, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 7858, "uuid": "ee7d3a6b6a1e4101b58538749b075030", "short_code": "instr", "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)", "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres." }, "relatedTo": { "ob_id": 10363, "uuid": "f5ca7b5b2e4f45b08b85f557cfe1528e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain Aircraft during Flight 00/24 over the Nottingham and Chesterfield Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } }, { "ob_id": 3481, "platform": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "instrument": { "ob_id": 8626, "uuid": "c069d0c60e0345b8b37d1c28adfb4db9", "short_code": "instr", "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)", "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present" }, "relatedTo": { "ob_id": 10363, "uuid": "f5ca7b5b2e4f45b08b85f557cfe1528e", "short_code": "acq", "title": "Acquisition Process for: Data from the CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain Aircraft during Flight 00/24 over the Nottingham and Chesterfield Areas", "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; " } } ] } ] }