{"count":14183,"next":"https://api.catalogue.ceda.ac.uk/api/v3/ipps/?format=json&limit=100&offset=3500","previous":"https://api.catalogue.ceda.ac.uk/api/v3/ipps/?format=json&limit=100&offset=3300","results":[{"ob_id":3502,"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":10395,"uuid":"7deb2609fe3e435fbfe652b7faa48713","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 02/22 over the Polden Hills 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":3503,"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":10399,"uuid":"d08977e306994bb79ee53cb3769d29a0","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 02/28 over the Avonmouth Smelter 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":3504,"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":10399,"uuid":"d08977e306994bb79ee53cb3769d29a0","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 02/28 over the Avonmouth Smelter 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":3505,"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":10399,"uuid":"d08977e306994bb79ee53cb3769d29a0","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 02/28 over the Avonmouth Smelter 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":3506,"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":10403,"uuid":"3f07f18c160a40ce888f914296ecdf33","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 02/29 over the Harper Adams 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":3507,"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":10403,"uuid":"3f07f18c160a40ce888f914296ecdf33","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 02/29 over the Harper Adams 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":3508,"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":10403,"uuid":"3f07f18c160a40ce888f914296ecdf33","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 02/29 over the Harper Adams 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":3509,"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":10407,"uuid":"41bfed47b3b04dbebcefff717644f929","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 02/30 over the Minstead and Highland Water Areas, New Forest","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":3510,"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":10407,"uuid":"41bfed47b3b04dbebcefff717644f929","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 02/30 over the Minstead and Highland Water Areas, New Forest","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":3511,"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":10407,"uuid":"41bfed47b3b04dbebcefff717644f929","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 02/30 over the Minstead and Highland Water Areas, New Forest","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":3512,"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":10411,"uuid":"6d4d2896e447446ea3c5d0eca6286b2e","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 02/31 over the Rothamsted 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":3513,"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":10411,"uuid":"6d4d2896e447446ea3c5d0eca6286b2e","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 02/31 over the Rothamsted 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":3514,"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":10411,"uuid":"6d4d2896e447446ea3c5d0eca6286b2e","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 02/31 over the Rothamsted 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":3515,"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":10415,"uuid":"96b3c31578534d3ba7c0c9466a0b0b79","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 02/34 over the Houghton le Spring 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":3516,"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":10415,"uuid":"96b3c31578534d3ba7c0c9466a0b0b79","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 02/34 over the Houghton le Spring 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":3517,"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":10415,"uuid":"96b3c31578534d3ba7c0c9466a0b0b79","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 02/34 over the Houghton le Spring 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":3518,"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":10419,"uuid":"7d3bd13680b641fe81a79062935527f0","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 02/43 over the Berwyn Mountains 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":3519,"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":10419,"uuid":"7d3bd13680b641fe81a79062935527f0","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 02/43 over the Berwyn Mountains 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":3520,"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":10423,"uuid":"c653208cf65047969a894abc800c96a7","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 97/13 over the Aspull and Coleorton 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), ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3521,"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":10423,"uuid":"c653208cf65047969a894abc800c96a7","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 97/13 over the Aspull and Coleorton 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), ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3522,"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":10423,"uuid":"c653208cf65047969a894abc800c96a7","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 97/13 over the Aspull and Coleorton 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), ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3523,"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":8701,"uuid":"0207b70a7b5543de832f5a0d49320cbe","short_code":"instr","title":"ARSF Compact Airbone Spectrographic Imager 1 (CASI-1)","abstract":"NERC ARSF Compact Airborne Spectrographic Imager 1"},"relatedTo":{"ob_id":10423,"uuid":"c653208cf65047969a894abc800c96a7","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 97/13 over the Aspull and Coleorton 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), ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3524,"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":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":10423,"uuid":"c653208cf65047969a894abc800c96a7","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 97/13 over the Aspull and Coleorton 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), ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3525,"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":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":10423,"uuid":"c653208cf65047969a894abc800c96a7","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 97/13 over the Aspull and Coleorton 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), ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3526,"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":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":10423,"uuid":"c653208cf65047969a894abc800c96a7","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 97/13 over the Aspull and Coleorton 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), ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3527,"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":8701,"uuid":"0207b70a7b5543de832f5a0d49320cbe","short_code":"instr","title":"ARSF Compact Airbone Spectrographic Imager 1 (CASI-1)","abstract":"NERC ARSF Compact Airborne Spectrographic Imager 1"},"relatedTo":{"ob_id":10423,"uuid":"c653208cf65047969a894abc800c96a7","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 97/13 over the Aspull and Coleorton 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), ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3528,"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":10427,"uuid":"fd7ecb0cfd834a1a85efe166ad8ce717","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 01/33 over the Myvatn Area, Iceland","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":3529,"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":10427,"uuid":"fd7ecb0cfd834a1a85efe166ad8ce717","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 01/33 over the Myvatn Area, Iceland","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":3530,"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":10427,"uuid":"fd7ecb0cfd834a1a85efe166ad8ce717","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 01/33 over the Myvatn Area, Iceland","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":3531,"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":10431,"uuid":"f3cebc12e1ed42f991ab87f06e94ef40","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 98/16 over Scolt Head Island, Tollesbury","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":3532,"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":10431,"uuid":"f3cebc12e1ed42f991ab87f06e94ef40","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 98/16 over Scolt Head Island, Tollesbury","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":3533,"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":10431,"uuid":"f3cebc12e1ed42f991ab87f06e94ef40","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 98/16 over Scolt Head Island, Tollesbury","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":3534,"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":10435,"uuid":"23ff610ecbd34eee91a76bdd32d1f95a","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 99/04 over the Lime Regis, The Pound, Eastbourne and Bembridge Areas","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, ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3535,"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":10435,"uuid":"23ff610ecbd34eee91a76bdd32d1f95a","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 99/04 over the Lime Regis, The Pound, Eastbourne and Bembridge Areas","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, ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3536,"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":10435,"uuid":"23ff610ecbd34eee91a76bdd32d1f95a","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 99/04 over the Lime Regis, The Pound, Eastbourne and Bembridge Areas","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, ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3537,"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":8701,"uuid":"0207b70a7b5543de832f5a0d49320cbe","short_code":"instr","title":"ARSF Compact Airbone Spectrographic Imager 1 (CASI-1)","abstract":"NERC ARSF Compact Airborne Spectrographic Imager 1"},"relatedTo":{"ob_id":10435,"uuid":"23ff610ecbd34eee91a76bdd32d1f95a","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 99/04 over the Lime Regis, The Pound, Eastbourne and Bembridge Areas","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, ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3538,"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":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":10435,"uuid":"23ff610ecbd34eee91a76bdd32d1f95a","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 99/04 over the Lime Regis, The Pound, Eastbourne and Bembridge Areas","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, ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3539,"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":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":10435,"uuid":"23ff610ecbd34eee91a76bdd32d1f95a","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 99/04 over the Lime Regis, The Pound, Eastbourne and Bembridge Areas","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, ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3540,"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":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":10435,"uuid":"23ff610ecbd34eee91a76bdd32d1f95a","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 99/04 over the Lime Regis, The Pound, Eastbourne and Bembridge Areas","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, ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3541,"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":8701,"uuid":"0207b70a7b5543de832f5a0d49320cbe","short_code":"instr","title":"ARSF Compact Airbone Spectrographic Imager 1 (CASI-1)","abstract":"NERC ARSF Compact Airborne Spectrographic Imager 1"},"relatedTo":{"ob_id":10435,"uuid":"23ff610ecbd34eee91a76bdd32d1f95a","short_code":"acq","title":"Acquisition Process for: Data from the Photographic Camera, CASI, CASI-2 and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft and the Dornier Do228-101 D-CALM Aircraft during Flight 99/04 over the Lime Regis, The Pound, Eastbourne and Bembridge Areas","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, ARSF Compact Airbone Spectrographic Imager 1 (CASI-1); PLATFORMS: Dornier Do228-101 D-CALM, Piper PA31 Navajo Chieftain G-NERC Aircraft; "}},{"ob_id":3542,"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":10439,"uuid":"9bbaa4f2cc704b3db6988742b62d8446","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 03/12 over the Finsterwalderbreen Area, Svalbard","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":3543,"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":10439,"uuid":"9bbaa4f2cc704b3db6988742b62d8446","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 03/12 over the Finsterwalderbreen Area, Svalbard","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":3544,"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":10439,"uuid":"9bbaa4f2cc704b3db6988742b62d8446","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 03/12 over the Finsterwalderbreen Area, Svalbard","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":3545,"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":10443,"uuid":"9bd7a8f1419e499e8d912d2c3ddb903c","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 03/19 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":3546,"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":10443,"uuid":"9bd7a8f1419e499e8d912d2c3ddb903c","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 03/19 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":3547,"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":10447,"uuid":"5e6d4b9b4b4b4a65abff555997f85d93","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 01/38 for Atmospheric Tests","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":3548,"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":10447,"uuid":"5e6d4b9b4b4b4a65abff555997f85d93","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 01/38 for Atmospheric Tests","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":3549,"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":10451,"uuid":"4c710d2b9da84c6f8e96344ec08c57dd","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 01/19 over the Grimsvotn Area, Icelane","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":3550,"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":10451,"uuid":"4c710d2b9da84c6f8e96344ec08c57dd","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 01/19 over the Grimsvotn Area, Icelane","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":3551,"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":10451,"uuid":"4c710d2b9da84c6f8e96344ec08c57dd","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 01/19 over the Grimsvotn Area, Icelane","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":3552,"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":10455,"uuid":"cf6c2727e6d341838ab8ba93eb37e05b","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 01/25 over the Salthouse Area, Norfolk Coast","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":3553,"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":10455,"uuid":"cf6c2727e6d341838ab8ba93eb37e05b","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 01/25 over the Salthouse Area, Norfolk Coast","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":3554,"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":10455,"uuid":"cf6c2727e6d341838ab8ba93eb37e05b","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 01/25 over the Salthouse Area, Norfolk Coast","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":3555,"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":10459,"uuid":"9d49ad6c135c45359561cad0ed1f7fc7","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 01/26 over the Mocatan 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":3556,"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":10459,"uuid":"9d49ad6c135c45359561cad0ed1f7fc7","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 01/26 over the Mocatan 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":3557,"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":10459,"uuid":"9d49ad6c135c45359561cad0ed1f7fc7","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 01/26 over the Mocatan 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":3558,"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":10463,"uuid":"06fb2ba08d2545818a9fe15e7652e01f","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 01/35 over the Jokulsa Area, Iceland","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":3559,"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":10463,"uuid":"06fb2ba08d2545818a9fe15e7652e01f","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 01/35 over the Jokulsa Area, Iceland","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":3560,"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":10463,"uuid":"06fb2ba08d2545818a9fe15e7652e01f","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 01/35 over the Jokulsa Area, Iceland","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":3561,"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":10467,"uuid":"0924dbbb424e442083ea4c92fdf831d9","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 01/36 over the Jarlhettur Area, Iceland","abstract":"This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; "}},{"ob_id":3562,"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":10467,"uuid":"0924dbbb424e442083ea4c92fdf831d9","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 01/36 over the Jarlhettur Area, Iceland","abstract":"This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; "}},{"ob_id":3563,"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":10467,"uuid":"0924dbbb424e442083ea4c92fdf831d9","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 01/36 over the Jarlhettur Area, Iceland","abstract":"This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; "}},{"ob_id":3564,"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":10471,"uuid":"f238139cee7645b6b7e9b3a596b8cba6","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 01/39 over the Thorney Island 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":3565,"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":10471,"uuid":"f238139cee7645b6b7e9b3a596b8cba6","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 01/39 over the Thorney Island 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":3566,"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":10471,"uuid":"f238139cee7645b6b7e9b3a596b8cba6","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 01/39 over the Thorney Island 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":3567,"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":10475,"uuid":"fc921eb323b84a36ab831716080efa02","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 01/44 over the Plymouth Algal Bloom","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":3568,"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":10475,"uuid":"fc921eb323b84a36ab831716080efa02","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 01/44 over the Plymouth Algal Bloom","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":3569,"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":10479,"uuid":"aa6bbde0a1144b618c238312bff99ec3","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 01/18 over the Langjokull Area, Iceland","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":3570,"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":10479,"uuid":"aa6bbde0a1144b618c238312bff99ec3","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 01/18 over the Langjokull Area, Iceland","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":3571,"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":10483,"uuid":"282da0204deb45559569039021f7c97d","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 01/34 over the Borgarfjordur Area, Iceland","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":3572,"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":10483,"uuid":"282da0204deb45559569039021f7c97d","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 01/34 over the Borgarfjordur Area, Iceland","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":3573,"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":10483,"uuid":"282da0204deb45559569039021f7c97d","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 01/34 over the Borgarfjordur Area, Iceland","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":3574,"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":10487,"uuid":"cb99a8980bc042d5b21af422c72799aa","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 01/16 over the Sorbas Basin Area, Spain","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":3575,"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":10487,"uuid":"cb99a8980bc042d5b21af422c72799aa","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 01/16 over the Sorbas Basin Area, Spain","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":3576,"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":10487,"uuid":"cb99a8980bc042d5b21af422c72799aa","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 01/16 over the Sorbas Basin Area, Spain","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":3577,"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":10491,"uuid":"25bab0a991e64d0d8d7b3dcde5fc8d1f","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 01/17 over the Butterwick Low 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":3578,"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":10491,"uuid":"25bab0a991e64d0d8d7b3dcde5fc8d1f","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 01/17 over the Butterwick Low 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":3579,"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":10491,"uuid":"25bab0a991e64d0d8d7b3dcde5fc8d1f","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 01/17 over the Butterwick Low 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":3580,"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":10495,"uuid":"734845e0607646179e85564e66c4ab4a","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 01/10 over the Tibberton 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 WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "}},{"ob_id":3581,"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":10495,"uuid":"734845e0607646179e85564e66c4ab4a","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 01/10 over the Tibberton 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 WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "}},{"ob_id":3582,"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":10495,"uuid":"734845e0607646179e85564e66c4ab4a","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 01/10 over the Tibberton 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 WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "}},{"ob_id":3583,"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":10499,"uuid":"2b7830a2f0e841d9bb0ba22807460d30","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 01/11 over the Menai Straits 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":3584,"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":10499,"uuid":"2b7830a2f0e841d9bb0ba22807460d30","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 01/11 over the Menai Straits 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":3585,"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":10503,"uuid":"d3b6a90c18744407bcaf5bfe849c3180","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 01/08 over the Rodaquilar Area, Spain","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":3586,"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":10503,"uuid":"d3b6a90c18744407bcaf5bfe849c3180","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 01/08 over the Rodaquilar Area, Spain","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":3587,"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":10503,"uuid":"d3b6a90c18744407bcaf5bfe849c3180","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 01/08 over the Rodaquilar Area, Spain","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":3588,"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":10507,"uuid":"36aea83660dc4b158b3e1ef00f5b346a","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 01/07 over the Rio de Ribadeo Area, Spain","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":3589,"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":10507,"uuid":"36aea83660dc4b158b3e1ef00f5b346a","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 01/07 over the Rio de Ribadeo Area, Spain","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":3590,"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":10511,"uuid":"447ec3fa16a94b00aeb413540f4b33f8","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 01/06 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":3591,"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":10511,"uuid":"447ec3fa16a94b00aeb413540f4b33f8","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 01/06 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":3592,"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":10511,"uuid":"447ec3fa16a94b00aeb413540f4b33f8","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 01/06 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":3593,"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":10515,"uuid":"38d88a4b9b904733b1565fb3b34c477b","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 01/04 over the Cors Caron Area","abstract":"This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; "}},{"ob_id":3594,"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":10515,"uuid":"38d88a4b9b904733b1565fb3b34c477b","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 01/04 over the Cors Caron Area","abstract":"This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; "}},{"ob_id":3595,"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":10515,"uuid":"38d88a4b9b904733b1565fb3b34c477b","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 01/04 over the Cors Caron Area","abstract":"This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; "}},{"ob_id":3596,"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":10519,"uuid":"b6e82183aeb045dda647cc47027ff085","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 01/15 over the New Forest 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":3597,"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":10519,"uuid":"b6e82183aeb045dda647cc47027ff085","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 01/15 over the New Forest 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":3598,"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":10519,"uuid":"b6e82183aeb045dda647cc47027ff085","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 01/15 over the New Forest 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":3599,"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":10523,"uuid":"dceadc6710e74aec85836e08973d9166","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 00/13 over the Rambla Castanos Area, Spain","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":3600,"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":10523,"uuid":"dceadc6710e74aec85836e08973d9166","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 00/13 over the Rambla Castanos Area, Spain","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":3601,"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":10523,"uuid":"dceadc6710e74aec85836e08973d9166","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 00/13 over the Rambla Castanos Area, Spain","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; "}}]}