Mobile Platform Operation List
Get a list of Mobile Platform Operation objects.
GET /api/v3/mpos/?format=api&offset=1500
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The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2246, "bboxName": "", "eastBoundLongitude": -0.39587000012397766, "westBoundLongitude": -6.386710166931152, "southBoundLatitude": 50.29758071899414, "northBoundLatitude": 52.37350845336914 }, "operationTime": { "ob_id": 7111, "startTime": "2018-02-20T00:00:00", "endTime": "2018-02-20T23:59:59" }, "childOperation": null }, { "ob_id": 26337, "uuid": "cae5dd627576459a9574f887be7bf7b3", "short_code": "mpop", "title": "FAAM BAE-147 flight C084", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C084. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2247, "bboxName": "", "eastBoundLongitude": -0.48456886410713196, "westBoundLongitude": -6.967024326324463, "southBoundLatitude": 51.22258758544922, "northBoundLatitude": 52.357879638671875 }, "operationTime": { "ob_id": 7112, "startTime": "2018-02-21T00:00:00", "endTime": "2018-02-21T23:59:59" }, "childOperation": null }, { "ob_id": 26341, "uuid": "fc81912ad79146779dd3178c616735e3", "short_code": "mpop", "title": "FAAM BAE-147 flight C085", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C085. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2248, "bboxName": "", "eastBoundLongitude": -131.75283813476562, "westBoundLongitude": -147.88290405273438, "southBoundLatitude": 64.80423736572266, "northBoundLatitude": 69.78407287597656 }, "operationTime": { "ob_id": 7113, "startTime": "2018-03-11T00:00:00", "endTime": "2018-03-11T23:59:59" }, "childOperation": null }, { "ob_id": 26345, "uuid": "9998089f30de41bb9352ac182c58208a", "short_code": "mpop", "title": "FAAM BAE-147 flight C086", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C086. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2249, "bboxName": "", "eastBoundLongitude": -147.50596618652344, "westBoundLongitude": -157.67431640625, "southBoundLatitude": 64.76835632324219, "northBoundLatitude": 71.31527709960938 }, "operationTime": { "ob_id": 7114, "startTime": "2018-03-13T00:00:00", "endTime": "2018-03-13T23:59:59" }, "childOperation": null }, { "ob_id": 26349, "uuid": "d3f8d2ecb52b4233a3ffab0bff813fb2", "short_code": "mpop", "title": "FAAM BAE-147 flight C087", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C087. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2250, "bboxName": "", "eastBoundLongitude": -132.68643188476562, "westBoundLongitude": -147.88543701171875, "southBoundLatitude": 64.80397033691406, "northBoundLatitude": 70.76052856445312 }, "operationTime": { "ob_id": 7115, "startTime": "2018-03-16T00:00:00", "endTime": "2018-03-16T23:59:59" }, "childOperation": null }, { "ob_id": 26353, "uuid": "669bf48a6db34c5e99141d72735a292d", "short_code": "mpop", "title": "FAAM BAE-147 flight C088", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C088. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2251, "bboxName": "", "eastBoundLongitude": -147.61294555664062, "westBoundLongitude": -156.39964294433594, "southBoundLatitude": 64.73687744140625, "northBoundLatitude": 70.37610626220703 }, "operationTime": { "ob_id": 7116, "startTime": "2018-03-17T00:00:00", "endTime": "2018-03-17T23:59:59" }, "childOperation": null }, { "ob_id": 26357, "uuid": "85e99c2441494a57bc440fff9dd4b034", "short_code": "mpop", "title": "FAAM BAE-147 flight C089", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C089. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2252, "bboxName": "", "eastBoundLongitude": -131.3230438232422, "westBoundLongitude": -148.18165588378906, "southBoundLatitude": 64.73011779785156, "northBoundLatitude": 69.11602020263672 }, "operationTime": { "ob_id": 7117, "startTime": "2018-03-18T14:20:50", "endTime": "2018-03-18T22:24:23" }, "childOperation": null }, { "ob_id": 26361, "uuid": "1c9b2ac39be54ad98d7f1a3ca6dfe057", "short_code": "mpop", "title": "FAAM BAE-147 flight C090", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C090. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2253, "bboxName": "", "eastBoundLongitude": -132.8860626220703, "westBoundLongitude": -147.88729858398438, "southBoundLatitude": 64.80281829833984, "northBoundLatitude": 69.81845092773438 }, "operationTime": { "ob_id": 7118, "startTime": "2018-03-20T00:00:00", "endTime": "2018-03-20T23:59:59" }, "childOperation": null }, { "ob_id": 26365, "uuid": "391950c93acb48fa8ef3b438545b036e", "short_code": "mpop", "title": "FAAM BAE-147 flight C091", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C091. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2254, "bboxName": "", "eastBoundLongitude": -147.6243438720703, "westBoundLongitude": -160.4109344482422, "southBoundLatitude": 64.72254180908203, "northBoundLatitude": 72.62899780273438 }, "operationTime": { "ob_id": 7119, "startTime": "2018-03-21T13:46:32", "endTime": "2018-03-21T22:00:45" }, "childOperation": null }, { "ob_id": 26369, "uuid": "a67fe4e908154f3ba884bbb4d6e5c2a6", "short_code": "mpop", "title": "FAAM BAE-147 flight C092", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C092. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2255, "bboxName": "", "eastBoundLongitude": -132.8597412109375, "westBoundLongitude": -148.15231323242188, "southBoundLatitude": 64.73310852050781, "northBoundLatitude": 70.82868957519531 }, "operationTime": { "ob_id": 7120, "startTime": "2018-03-22T00:00:00", "endTime": "2018-03-22T23:59:59" }, "childOperation": null }, { "ob_id": 26373, "uuid": "e84d64e1678d48c784e91840f973d88b", "short_code": "mpop", "title": "FAAM BAE-147 flight C093", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C093. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2256, "bboxName": "", "eastBoundLongitude": -147.60665893554688, "westBoundLongitude": -160.2390899658203, "southBoundLatitude": 64.67627716064453, "northBoundLatitude": 69.54341125488281 }, "operationTime": { "ob_id": 7121, "startTime": "2018-03-23T00:00:00", "endTime": "2018-03-23T23:59:59" }, "childOperation": null }, { "ob_id": 26377, "uuid": "705be0ddf4634e90883e50b6a27d77d2", "short_code": "mpop", "title": "FAAM BAE-147 flight C096", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C096. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2257, "bboxName": "", "eastBoundLongitude": 2.9532461166381836, "westBoundLongitude": -0.6888627409934998, "southBoundLatitude": 52.041385650634766, "northBoundLatitude": 53.42739486694336 }, "operationTime": { "ob_id": 7122, "startTime": "2018-04-20T08:24:32", "endTime": "2018-04-20T14:30:34" }, "childOperation": null }, { "ob_id": 26381, "uuid": "9d0337229b5c4aa0a0cb339e317b3231", "short_code": "mpop", "title": "FAAM BAE-147 flight C095", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C095. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2258, "bboxName": "", "eastBoundLongitude": 2.940340042114258, "westBoundLongitude": -0.7029100060462952, "southBoundLatitude": 52.03376007080078, "northBoundLatitude": 54.77265167236328 }, "operationTime": { "ob_id": 7123, "startTime": "2018-04-18T23:00:00", "endTime": "2018-04-19T22:59:59" }, "childOperation": null }, { "ob_id": 26385, "uuid": "5a0054dd82c0483f84ed5f7a8c38554c", "short_code": "mpop", "title": "FAAM BAE-147 flight C094", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C094. 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The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2259, "bboxName": "", "eastBoundLongitude": -0.37922999262809753, "westBoundLongitude": -7.286640167236328, "southBoundLatitude": 49.909629821777344, "northBoundLatitude": 52.382301330566406 }, "operationTime": { "ob_id": 7124, "startTime": "2018-04-12T23:00:00", "endTime": "2018-04-13T22:59:59" }, "childOperation": null }, { "ob_id": 26389, "uuid": "8ea0c3365a234ef09a3f1c5f066bc264", "short_code": "mpop", "title": "FAAM BAE-147 flight C097", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C097. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2260, "bboxName": "", "eastBoundLongitude": -0.3922654986381531, "westBoundLongitude": -3.7558326721191406, "southBoundLatitude": 50.9835205078125, "northBoundLatitude": 52.37442398071289 }, "operationTime": { "ob_id": 7125, "startTime": "2018-04-23T04:26:25", "endTime": "2018-04-23T11:45:27" }, "childOperation": null }, { "ob_id": 26393, "uuid": "ea8715d89e4b41d0953791ce965989d1", "short_code": "mpop", "title": "FAAM BAE-147 flight C098", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C098. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. 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The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2319, "bboxName": "", "eastBoundLongitude": 2.200350046157837, "westBoundLongitude": -0.6249210238456726, "southBoundLatitude": 52.06529998779297, "northBoundLatitude": 53.69329833984375 }, "operationTime": { "ob_id": 7253, "startTime": "2018-09-06T04:47:26", "endTime": "2018-09-06T10:45:02" }, "childOperation": null }, { "ob_id": 26947, "uuid": "0f78ae10450649d3b452ed3a93c75d94", "short_code": "mpop", "title": "FAAM BAE-147 flight C116", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C116. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2320, "bboxName": "", "eastBoundLongitude": 0.4724510610103607, "westBoundLongitude": -0.8405385613441467, "southBoundLatitude": 52.039222717285156, "northBoundLatitude": 54.59601974487305 }, "operationTime": { "ob_id": 7254, "startTime": "2018-09-07T05:39:33.900391", "endTime": "2018-09-07T11:12:35.898438" }, "childOperation": null }, { "ob_id": 26951, "uuid": "6bbae78956a445d5a8b07216ea7054ce", "short_code": "mpop", "title": "FAAM BAE-147 flight C117", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C117. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2321, "bboxName": "", "eastBoundLongitude": -1.6099677085876465, "westBoundLongitude": -4.204505443572998, "southBoundLatitude": 58.43046569824219, "northBoundLatitude": 60.65217208862305 }, "operationTime": { "ob_id": 7255, "startTime": "2018-09-10T09:49:16", "endTime": "2018-09-10T15:26:33" }, "childOperation": null }, { "ob_id": 26955, "uuid": "f65994a39fe94a76a69ceee100661024", "short_code": "mpop", "title": "FAAM BAE-147 flight C118", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C118. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2322, "bboxName": "", "eastBoundLongitude": -2.3963029384613037, "westBoundLongitude": -4.428136825561523, "southBoundLatitude": 58.43247985839844, "northBoundLatitude": 61.07949447631836 }, "operationTime": { "ob_id": 7256, "startTime": "2018-09-11T06:18:02", "endTime": "2018-09-11T12:30:23" }, "childOperation": null }, { "ob_id": 26959, "uuid": "8de41db1a43f497193d69062ed8e96f9", "short_code": "mpop", "title": "FAAM BAE-147 flight C119", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C119. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2323, "bboxName": "", "eastBoundLongitude": 1.6245050430297852, "westBoundLongitude": -3.291314125061035, "southBoundLatitude": 57.1961784362793, "northBoundLatitude": 58.500179290771484 }, "operationTime": { "ob_id": 7257, "startTime": "2018-09-11T12:45:32", "endTime": "2018-09-11T17:14:14" }, "childOperation": null }, { "ob_id": 26963, "uuid": "16e9598ac8a74ea59202219333e0d691", "short_code": "mpop", "title": "FAAM BAE-147 flight C120", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C120. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2324, "bboxName": "", "eastBoundLongitude": -1.2020186185836792, "westBoundLongitude": -4.172128200531006, "southBoundLatitude": 57.02179718017578, "northBoundLatitude": 60.69862365722656 }, "operationTime": { "ob_id": 7258, "startTime": "2018-09-12T07:07:22", "endTime": "2018-09-12T14:43:24" }, "childOperation": null }, { "ob_id": 26967, "uuid": "2c1b0a2afec343fe9dc87d4ba1707fcd", "short_code": "mpop", "title": "FAAM BAE-147 flight C122", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C122. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2325, "bboxName": "", "eastBoundLongitude": 2.191499948501587, "westBoundLongitude": -0.6793379783630371, "southBoundLatitude": 50.788299560546875, "northBoundLatitude": 52.89419937133789 }, "operationTime": { "ob_id": 7259, "startTime": "2018-12-12T08:20:49", "endTime": "2018-12-12T15:01:21" }, "childOperation": null }, { "ob_id": 26971, "uuid": "903bcfc3e08c4d4da8c8e307b310c734", "short_code": "mpop", "title": "FAAM BAE-147 flight C126", "abstract": "Flight details for FAAM BAE-146 aircraft flight number C126. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 51, "uuid": "dda4596d5d374564acf8c79b7a119127", "short_code": "plat", "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE", "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis" }, "location": { "ob_id": 2326, "bboxName": "", "eastBoundLongitude": -0.3961317241191864, "westBoundLongitude": -6.215221405029297, "southBoundLatitude": 50.74294662475586, "northBoundLatitude": 52.373043060302734 }, "operationTime": { "ob_id": 7260, "startTime": "2019-01-09T09:33:51", "endTime": "2019-01-09T17:16:08" }, "childOperation": null }, { "ob_id": 27132, "uuid": "6c74884699f541ff8a1edb33933ddada", "short_code": "mpop", "title": "Coriolis Satellite Orbit Details", "abstract": "The Coriolis Satellite is flown by NASA and the US Department of Defence and is in a Sunsynchronous orbit with an 06.10 descending equator crossing time.", "status": "", "platform_field": { "ob_id": 27130, "uuid": "526c6fb02e094d049d367aaa4f79e8d1", "short_code": "plat", "title": "Coriolis", "abstract": "The Coriolis satellite is flown by NASA and the US Department of Defence, with a primary mission to provide observations of the sea-surface wind. It carries two instruments: WindSat and SMEI (Solar Mass Ejection Imager)" }, "location": null, "operationTime": null, "childOperation": null }, { "ob_id": 27133, "uuid": "c15fb49dfbf24bdc81acb5ae16df1b1d", "short_code": "mpop", "title": "SMOS satellite orbit details", "abstract": "The SMOS satellite is operated by ESA and is in a sunscynchronous orbit with a 06:00 ascending equator crossing time.", "status": "", "platform_field": { "ob_id": 27128, "uuid": "9c6e8c73f539446ba7a8adef871492a7", "short_code": "plat", "title": "SMOS", "abstract": "The SMOS (Soil Moisture and Ocean Salinity) satellite was launched on Novermber 2009, with the primary mission to monitor ocean salinity and soil moisture." }, "location": null, "operationTime": null, "childOperation": null }, { "ob_id": 27137, "uuid": "f6550c6efe0c4a9baaf3c5d07627b2ed", "short_code": "mpop", "title": "GCOM-W satellite orbit details", "abstract": "The GCOM-W (Global Change Observation Mission for Water) is a JAXA satellite in a sunsynchronous orbit with a 13.30 ascending equator crossing time.", "status": "", "platform_field": { "ob_id": 25273, "uuid": "f10d619f7b9f4dbab792dcc1ab9dbb68", "short_code": "plat", "title": "GCOM-W (Global Change Observation Mission for Water)", "abstract": "The Global Change Observation Mission for Water (GCOM-W) is a series of three satellites flown by the Japanese Space Agency (JAXA), addressing multi-purpose MW imagery for ocean, land and precipitation. It is part of their Global Change Observation Mission (GCOM).\r\nThe satellites exploit sun-synchronous orbits around 13:30, coordinated with that of POES satellites, Suomi-NPP and JPSS." }, "location": null, "operationTime": null, "childOperation": null }, { "ob_id": 27138, "uuid": "44f2493522254d2696575ce3acb6146c", "short_code": "mpop", "title": "TRMM satellite orbit details", "abstract": "The TRMM (Tropical Rainfall Measuring Mission) is a NASA, JAXA satellite mission. It is in a drifting orbit with an inclination of 35 degrees and altitude of 402 km.", "status": "", "platform_field": { "ob_id": 27135, "uuid": "8afe985a2f3f4b15aaa52df6119c0f27", "short_code": "plat", "title": "TRMM", "abstract": "The Tropical Rainfall Measuring Mission (TRMM) is a NASA and JAXA satellite that flew between 1997 and 2015. It's primary mission was to measure precipitation." }, "location": null, "operationTime": null, "childOperation": null }, { "ob_id": 27176, "uuid": "3dbc37a5c3654042bafc881e45cfe095", "short_code": "mpop", "title": "Mobile Platform Operation for: NOAA-18", "abstract": "Mobile Platform Operation related to the: NOAA-18", "status": "", "platform_field": { "ob_id": 27174, "uuid": "3dba7abe842a4f55b7d27d58cfa6b7ac", "short_code": "plat", "title": "NOAA-18", "abstract": "NOAA (National Oceanic and Atmospheric Administration) polar orbiting satellite which was launched on 20th May, 2005." }, "location": null, "operationTime": null, "childOperation": null }, { "ob_id": 27177, "uuid": "c39c76fd8d8f4823b8ff6533a0d96a10", "short_code": "mpop", "title": "Mobile Platform Operation for: NOAA-19", "abstract": "Mobile Platform Operation related to the: NOAA-19", "status": "", "platform_field": { "ob_id": 27175, "uuid": "c6470e63d7f84f20b9c765be3d0b9352", "short_code": "plat", "title": "NOAA-19", "abstract": "NOAA (National Oceanic and Atmospheric Administration) polar orbiting satellite which was launched on 6th February 2009" }, "location": null, "operationTime": null, "childOperation": null }, { "ob_id": 27631, "uuid": "a385d6248689489382c7569cebd0e3bd", "short_code": "mpop", "title": "ARSF flight 2014_309", "abstract": "ARSF flight 2014_309", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2410, "bboxName": "ARSF flight 2014-309", "eastBoundLongitude": 118.02, "westBoundLongitude": 117.88, "southBoundLatitude": 5.79, "northBoundLatitude": 5.88 }, "operationTime": { "ob_id": 7403, "startTime": "2014-11-05T00:00:00", "endTime": "2014-11-06T00:00:00" }, "childOperation": null }, { "ob_id": 27743, "uuid": "86bd9adc06eb4c979e790b213cf97bdd", "short_code": "mpop", "title": "Mobile Platform Operation for: Defense Meteorological Satellite Program (DMSP) Satellites - F11", "abstract": "Mobile Platform Operation related to the: Defense Meteorological Satellite Program (DMSP) Satellites", "status": "", "platform_field": { "ob_id": 27698, "uuid": "d001dfe5f77b498084b6d35bc0412af0", "short_code": "plat", "title": "Defense Meteorological Satellite Program - F11", "abstract": "11th flight unit of the DMSP Block 5D series, 6th of the Block 5D-2 series. Main missions: cloud imagery and MW imaging and temperature/humidity sounding. Substantial contribution to Space weather." }, "location": null, "operationTime": null, "childOperation": null }, { "ob_id": 27744, "uuid": "69948c81ccb945f79fe7631faec1a348", "short_code": "mpop", "title": "Mobile Platform Operation for: Defense Meteorological Satellite Program (DMSP) Satellites - F12", "abstract": "Mobile Platform Operation related to the: Defense Meteorological Satellite Program (DMSP) Satellites", "status": "", "platform_field": { "ob_id": 27699, "uuid": "d41601bebc634548bb85c1c645221c83", "short_code": "plat", "title": "Defense Meteorological Satellite Program - F12", "abstract": "12th flight unit of the DMSP Block 5D series, 6th of the Block 5D-2 series. Main missions: cloud imagery and MW imaging and temperature/humidity sounding. Substantial contribution to Space weather." }, "location": null, "operationTime": null, "childOperation": null }, { "ob_id": 27745, "uuid": "64065762387d46e5aa10e17b38ffebd6", "short_code": "mpop", "title": "Mobile Platform Operation for: Defense Meteorological Satellite Program (DMSP) Satellites - F14", "abstract": "Mobile Platform Operation related to the: Defense Meteorological Satellite Program (DMSP) Satellites", "status": "", "platform_field": { "ob_id": 27700, "uuid": "acda9a20482b4aa0833231df4ada0e05", "short_code": "plat", "title": "Defense Meteorological Satellite Program - F14", "abstract": "14th flight unit of the DMSP Block 5D series, 6th of the Block 5D-2 series. Main missions: cloud imagery and MW imaging and temperature/humidity sounding. Substantial contribution to Space weather." }, "location": null, "operationTime": null, "childOperation": null }, { "ob_id": 27746, "uuid": "008956ddb7834ef4923337840b95d033", "short_code": "mpop", "title": "Mobile Platform Operation for: Defense Meteorological Satellite Program (DMSP) Satellites - F15", "abstract": "Mobile Platform Operation related to the: Defense Meteorological Satellite Program (DMSP) Satellites", "status": "", "platform_field": { "ob_id": 27701, "uuid": "aa5c0c3f0339443aa92e15763bc07256", "short_code": "plat", "title": "Defense Meteorological Satellite Program - F15", "abstract": "15th flight unit of the DMSP Block 5D series, 6th of the Block 5D-2 series. Main missions: cloud imagery and MW imaging and temperature/humidity sounding. Substantial contribution to Space weather." }, "location": null, "operationTime": null, "childOperation": null }, { "ob_id": 28025, "uuid": "64b82a154b5c43f4888db80d62843ad4", "short_code": "mpop", "title": "Mobile Platform Operation for GOSAT", "abstract": "Mobile Platform Operation for GOSAT", "status": "ongoing", "platform_field": { "ob_id": 28024, "uuid": "82c8982483b3474390df11067f7d267b", "short_code": "plat", "title": "GOSAT", "abstract": "The Greenhouse Gas Observing Satellite (GOSAT) observes infrared light reflected and emitted from the earth's surface and the atmosphere. Column abundances of CO2 and CH4 are calculated from the observational data. The column abundance of a gas species is expressed as the number of the gas molecules in a column above a unit surface area. GOSAT is a Japanese satellite that flies at an altitude\r\nof approximately 666 km and completes one revolution in about 100 minutes. The satellite returns to the same point in space in three days. The observation instrument onboard the satellite is the Thermal And Near-infrared Sensor for carbon Observation (TANSO). TANSO is composed of two subunits: the Fourier Transform Spectrometer (FTS) and the Cloud and Aerosol Imager (CAI)." }, "location": null, "operationTime": { "ob_id": 7532, "startTime": "2009-01-23T00:00:00", "endTime": null }, "childOperation": null }, { "ob_id": 28058, "uuid": "e3cc8e64e4b54532b86f46c19632765f", "short_code": "mpop", "title": "ARSF 2013_198 - IG13_21 Flight", "abstract": "ARSF 2013_198 - IG13_21 Flight - over Helheim Glacier", "status": "", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2536, "bboxName": "ARSF flight 2013-198", "eastBoundLongitude": -37.0, "westBoundLongitude": -38.77, "southBoundLatitude": 65.54, "northBoundLatitude": 66.62 }, "operationTime": null, "childOperation": null }, { "ob_id": 28071, "uuid": "21a36bd7aafe42a19871189ceb5854ec", "short_code": "mpop", "title": "ARSF 2013_222a - IG13_21 Flight", "abstract": "ARSF 2013_222a - IG13_21 Flight - Helheim Glacier, Greenland", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2540, "bboxName": "ARSF flight 222 a and b", "eastBoundLongitude": -37.94, "westBoundLongitude": -38.61, "southBoundLatitude": 66.23, "northBoundLatitude": 66.54 }, "operationTime": null, "childOperation": null }, { "ob_id": 28076, "uuid": "34092d94b3d94f54a02d356910d0bd02", "short_code": "mpop", "title": "ARSF 2013_223 - IG13_21", "abstract": "ARSF 2013_223 flight for IG13_21", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2542, "bboxName": "ARSF flight 2013_223", "eastBoundLongitude": -38.0, "westBoundLongitude": -38.33, "southBoundLatitude": 66.3, "northBoundLatitude": 66.4 }, "operationTime": null, "childOperation": null }, { "ob_id": 28077, "uuid": "5088c90e227548ba8e6c455fadbbc1c9", "short_code": "mpop", "title": "ARSF 2013_222b -IG13_21", "abstract": "ARSF 2013_222b flight for IG13_21", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2540, "bboxName": "ARSF flight 222 a and b", "eastBoundLongitude": -37.94, "westBoundLongitude": -38.61, "southBoundLatitude": 66.23, "northBoundLatitude": 66.54 }, "operationTime": null, "childOperation": null }, { "ob_id": 28078, "uuid": "797113fabf114785a7cc45369195e47a", "short_code": "mpop", "title": "ARSF 2013_221 - IG13_21", "abstract": "ARSF 2013_221 - IG13_21 Helheim Glacier Greenland", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2539, "bboxName": "ARSF flight 2013_221", "eastBoundLongitude": -38.05, "westBoundLongitude": -38.57, "southBoundLatitude": 66.3, "northBoundLatitude": 66.5 }, "operationTime": null, "childOperation": null }, { "ob_id": 29927, "uuid": "55ed74e1a1fb46f3ac06744ea422a795", "short_code": "mpop", "title": "Mobile Platform Operation for: OrbView-2 (SeaStar)", "abstract": "The SeaStar spacecraft, developed by Orbital Sciences Corporation, carries the SeaWiFS instrument and was launched to low Earth orbit on board an extended Pegasus launch vehicle on August 1, 1997. The SeaWiFS instrument will be the only scientific payload on the SeaStar spacecraft. GeoEye has the sole responsibility for the command and control of the satellite. The development of the SeaWiFS instrument was subcontracted to Hughes/SBRC, but GeoEye maintains ultimate responsibility for the instrument.", "status": "", "platform_field": { "ob_id": 29925, "uuid": "65c32f4b87db4448bec5f5b52a328cde", "short_code": "plat", "title": "OrbView-2", "abstract": "OrbView 2, also known as SeaStar, is a commercial Earth observation satellite, which operates its SeaWiFS sensor for NASA. On 11 December 2010, after more than 13 years, the communication with the instrument ceased." }, "location": { "ob_id": 529, "bboxName": "Global (-180 to 180)", "eastBoundLongitude": 180.0, "westBoundLongitude": -180.0, "southBoundLatitude": -90.0, "northBoundLatitude": 90.0 }, "operationTime": { "ob_id": 8137, "startTime": "1997-07-31T23:00:00", "endTime": "2010-12-11T00:00:00" }, "childOperation": null }, { "ob_id": 31686, "uuid": "3977d716314349cb8f2aaf4114c7de82", "short_code": "mpop", "title": "ARSF flight 2014_293", "abstract": "Flight details for NERC-ARSF aircraft flight number 2014_293. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2673, "bboxName": "", "eastBoundLongitude": 117.66891853215606, "westBoundLongitude": 117.5493594242588, "southBoundLatitude": 4.620428057219033, "northBoundLatitude": 4.775620568370908 }, "operationTime": { "ob_id": 8672, "startTime": "2014-10-20T23:12:50", "endTime": "2014-10-21T02:54:41" }, "childOperation": null }, { "ob_id": 31690, "uuid": "13c546da1b6a4021ba20a8c7dffd233a", "short_code": "mpop", "title": "ARSF flight ARSF2014_291", "abstract": "Flight details for NERC-ARSF aircraft flight number ARSF2014_291. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2674, "bboxName": "", "eastBoundLongitude": 117.58766488346275, "westBoundLongitude": 117.47908274364123, "southBoundLatitude": 4.537965016884551, "northBoundLatitude": 4.730123229864012 }, "operationTime": { "ob_id": 8673, "startTime": "2014-10-18T00:52:07", "endTime": "2014-10-18T01:58:20" }, "childOperation": null }, { "ob_id": 31694, "uuid": "7664e71dc2f445d5975a3d5521c436f8", "short_code": "mpop", "title": "ARSF flight ARSF2014_290", "abstract": "Flight details for NERC-ARSF aircraft flight number ARSF2014_290. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2675, "bboxName": "", "eastBoundLongitude": 117.70125347067703, "westBoundLongitude": 117.40626245827607, "southBoundLatitude": 4.592539196112926, "northBoundLatitude": 4.811220500698796 }, "operationTime": { "ob_id": 8674, "startTime": "2014-10-17T00:31:29", "endTime": "2014-10-17T03:04:12" }, "childOperation": null }, { "ob_id": 31698, "uuid": "aa2adc204d21489280a345544e253fda", "short_code": "mpop", "title": "ARSF flight ARSF2014_288", "abstract": "Flight details for NERC-ARSF aircraft flight number ARSF2014_288. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2676, "bboxName": "", "eastBoundLongitude": 117.70338088257677, "westBoundLongitude": 117.39879269878887, "southBoundLatitude": 4.587674017023778, "northBoundLatitude": 4.816019734940055 }, "operationTime": { "ob_id": 8675, "startTime": "2014-10-15T00:40:17", "endTime": "2014-10-15T02:53:38" }, "childOperation": null }, { "ob_id": 31702, "uuid": "913fcd87955d4908a2335c7d42ec5f27", "short_code": "mpop", "title": "ARSF flight ARSF2014_289", "abstract": "Flight details for NERC-ARSF aircraft flight number ARSF2014_289. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2677, "bboxName": "", "eastBoundLongitude": 117.74246049955697, "westBoundLongitude": 117.41424923888636, "southBoundLatitude": 4.580747175389046, "northBoundLatitude": 4.797325657640901 }, "operationTime": { "ob_id": 8676, "startTime": "2014-10-16T00:03:50", "endTime": "2014-10-16T02:07:40" }, "childOperation": null }, { "ob_id": 31706, "uuid": "df4af2432dff4411b56600e2bc32031b", "short_code": "mpop", "title": "ARSF flight ARSF2014_294", "abstract": "Flight details for NERC-ARSF aircraft flight number ARSF2014_294. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2678, "bboxName": "", "eastBoundLongitude": 117.55063263075196, "westBoundLongitude": 117.51495982362353, "southBoundLatitude": 4.552048288535308, "northBoundLatitude": 4.736545185985469 }, "operationTime": { "ob_id": 8677, "startTime": "2014-10-21T23:49:02", "endTime": "2014-10-22T01:59:25" }, "childOperation": null }, { "ob_id": 31710, "uuid": "4dd41cd851834953ab3b63ec05d79567", "short_code": "mpop", "title": "ARSF flight ARSF2014_295", "abstract": "Flight details for NERC-ARSF aircraft flight number ARSF2014_295. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2679, "bboxName": "", "eastBoundLongitude": 117.49188884850399, "westBoundLongitude": 117.40263608929236, "southBoundLatitude": 4.618881134382001, "northBoundLatitude": 4.804893836457523 }, "operationTime": { "ob_id": 8678, "startTime": "2014-10-22T23:08:02", "endTime": "2014-10-23T01:58:13" }, "childOperation": null }, { "ob_id": 31714, "uuid": "388d35496ea64d8bb71b1751ea6ade5f", "short_code": "mpop", "title": "ARSF flight ARSF2014_297", "abstract": "Flight details for NERC-ARSF aircraft flight number ARSF2014_297. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2680, "bboxName": "", "eastBoundLongitude": 117.48817633899782, "westBoundLongitude": 117.39349203019951, "southBoundLatitude": 4.5932506485855225, "northBoundLatitude": 4.749846309445186 }, "operationTime": { "ob_id": 8679, "startTime": "2014-10-24T23:21:19", "endTime": "2014-10-25T02:11:47" }, "childOperation": null }, { "ob_id": 31718, "uuid": "5283b87a332947d5a13aa7164fb7fa01", "short_code": "mpop", "title": "ARSF flight ARSF2014_298", "abstract": "Flight details for NERC-ARSF aircraft flight number ARSF2014_298. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2681, "bboxName": "", "eastBoundLongitude": 117.71558375687995, "westBoundLongitude": 117.51381931655933, "southBoundLatitude": 4.5924582311762325, "northBoundLatitude": 4.8002555119741475 }, "operationTime": { "ob_id": 8680, "startTime": "2014-10-25T23:04:42", "endTime": "2014-10-26T02:00:11" }, "childOperation": null }, { "ob_id": 31722, "uuid": "4f8d72f0b9af4424bf8e73261c21a356", "short_code": "mpop", "title": "ARSF flight ARSF2014_302a", "abstract": "Flight details for NERC-ARSF aircraft flight number ARSF2014_302a. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2682, "bboxName": "", "eastBoundLongitude": 116.97837277926037, "westBoundLongitude": 116.95109582338233, "southBoundLatitude": 4.739585665218536, "northBoundLatitude": 4.76003852152338 }, "operationTime": { "ob_id": 8681, "startTime": "2014-11-01T00:50:57", "endTime": "2014-11-01T01:12:10" }, "childOperation": null }, { "ob_id": 31726, "uuid": "9a87286ca3d54b4ab17925f8c80d8e9d", "short_code": "mpop", "title": "ARSF flight ARSF2014_303", "abstract": "Flight details for NERC-ARSF aircraft flight number ARSF2014_303. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2683, "bboxName": "", "eastBoundLongitude": 116.96895546805689, "westBoundLongitude": 116.92445895305372, "southBoundLatitude": 4.719108755815142, "northBoundLatitude": 4.772706413504848 }, "operationTime": { "ob_id": 8682, "startTime": "2014-10-30T23:30:55", "endTime": "2014-10-31T01:27:23" }, "childOperation": null }, { "ob_id": 32133, "uuid": "3282d841bba742e699cddd6d91327953", "short_code": "mpop", "title": "Mobile Platform Operation for: Metop-C", "abstract": "Mobile Platform Operation related to the: Metop-C", "status": "ongoing", "platform_field": { "ob_id": 32134, "uuid": "db86d823aded474e8c76bd69d092d26b", "short_code": "plat", "title": "Metop-C", "abstract": "Metop-C launched on 7th November 2018, represents the first in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS). Metop-C is Europe's third polar-orbiting meteorological satellite" }, "location": { "ob_id": 529, "bboxName": "Global (-180 to 180)", "eastBoundLongitude": 180.0, "westBoundLongitude": -180.0, "southBoundLatitude": -90.0, "northBoundLatitude": 90.0 }, "operationTime": { "ob_id": 8815, "startTime": "2018-11-07T00:00:00", "endTime": null }, "childOperation": null }, { "ob_id": 32275, "uuid": "4e0e67f525184a0081e607c2c15f4707", "short_code": "mpop", "title": "ARSF flight 2019_168", "abstract": "Flight details for NERC-ARSF aircraft flight number 2019_168. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2742, "bboxName": "", "eastBoundLongitude": 11.07996281264967, "westBoundLongitude": 10.986786122783649, "southBoundLatitude": 42.675919524996075, "northBoundLatitude": 42.8701064765462 }, "operationTime": { "ob_id": 8854, "startTime": "2019-06-17T09:02:03", "endTime": "2019-06-17T09:59:10" }, "childOperation": null }, { "ob_id": 32280, "uuid": "380f9c7afcc643968fc995be7554bc83", "short_code": "mpop", "title": "ARSF flight 2019_169", "abstract": "Flight details for NERC-ARSF aircraft flight number 2019_169. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2743, "bboxName": "", "eastBoundLongitude": 10.801836378669647, "westBoundLongitude": 10.792696888648972, "southBoundLatitude": 42.677424990857055, "northBoundLatitude": 43.205923744277996 }, "operationTime": { "ob_id": 8855, "startTime": "2019-06-18T08:12:09", "endTime": "2019-06-18T10:13:30" }, "childOperation": null }, { "ob_id": 32319, "uuid": "ef9e022c55f84b8ba4c4bc899d8c471f", "short_code": "mpop", "title": "ARSF flight 2019_171a", "abstract": "Flight details for NERC-ARSF aircraft flight number 2019_171a. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 6394, "uuid": "d2c5c36981824b71a98a2906394d61f3", "short_code": "plat", "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft", "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n Speed:\r\n Min speed: 62 m/s\r\n Max speed: 83 m/s\r\n Usual speed during measurements: 65 m/s\r\n Usual speed during transit flights: 98 m/s\r\n Ascent rate: 1000 m/s\r\n\r\n Altitude:\r\n (1 ft = 0.31 m)\r\n Min altitude:\r\n Above sea: 200 ft\r\n Above ground: 500 ft\r\n Max ceiling: 22000 ft\r\n Usual ceiling during measurements: 15000 ft\r\n Ceiling limitations:\r\n The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n Payload:\r\n Empty weight: 3596 kg\r\n Max take-off weight: 5980 kg\r\n Max payload: 1595 kg\r\n Usual scientific payload during measurements: 500 kg\r\n Endurance:\r\n Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n \t\r\n Range:\r\n Max range: 2600 km (at min scientific payload and max fuel)\r\n Conditions for max range:\r\n FL150 at max fuel, speed = 180 KTAS\r\n Range at max scientific payload: 1800 km\r\n Usual range during measurement flight: 1500 km\r\n\r\n Other:\r\n Weather conditions limitations:\r\n VFR/IFR Approved Certified to fly in known icing conditions\r\n Take-off runway length: 625 m\r\n Engines:\r\n twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n Avionics:\r\n INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n Apertures:\r\n Cargo door:\r\n Width : 1.28 m\r\n Height : 1.34 m;\r\n Cabin pressurized:\r\n none\r\n More information:\r\n Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n Nose boom:\r\n none\r\n Windows:\r\n 2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n Openings:\r\n Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n Hard points:\r\n Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n Inlets:\r\n One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n Additional systems:\r\n From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n Leica ALS 50-II Lidar\r\n Leica RCD-105 39 Mega Pixel Digital Camera\r\n Specim Eagle & Hawk Hyperspectral Scanner\r\n Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n Aircraft total electrical power (kW):\r\n 28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n Electrical power (kW) and voltages (V) available for scientists:\r\n DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter " }, "location": { "ob_id": 2744, "bboxName": "", "eastBoundLongitude": 11.26207356990549, "westBoundLongitude": 10.961480973176984, "southBoundLatitude": 42.61179553279232, "northBoundLatitude": 43.27429746092267 }, "operationTime": { "ob_id": 8861, "startTime": "2019-06-20T07:11:09", "endTime": "2019-06-20T08:09:00" }, "childOperation": null }, { "ob_id": 32323, "uuid": "1ad030ab2b8f49a3b7c5eaa388759cf0", "short_code": "mpop", "title": "NERC-ARF flight 2019_171a", "abstract": "Flight details for NERC-ARF aircraft flight number 2019_171a. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2745, "bboxName": "", "eastBoundLongitude": 11.26207356990549, "westBoundLongitude": 10.961480973176984, "southBoundLatitude": 42.61179553279232, "northBoundLatitude": 43.27429746092267 }, "operationTime": { "ob_id": 8862, "startTime": "2019-06-20T07:11:09", "endTime": "2019-06-20T08:09:00" }, "childOperation": null }, { "ob_id": 32435, "uuid": "67fd8c834def489da2aaf3d10b44ea9e", "short_code": "mpop", "title": "NERC-ARF flight 2018_123", "abstract": "Flight details for NERC-ARF aircraft flight number 2018_123. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2746, "bboxName": "", "eastBoundLongitude": -0.3629166097637084, "westBoundLongitude": -0.39727101512377117, "southBoundLatitude": 51.80004192491934, "northBoundLatitude": 51.822618533045386 }, "operationTime": { "ob_id": 8910, "startTime": "2018-05-03T14:44:56", "endTime": "2018-05-03T14:56:29" }, "childOperation": null }, { "ob_id": 32443, "uuid": "f26918281177475dbe7a846d117ce079", "short_code": "mpop", "title": "NERC-ARF flight 2018_135a", "abstract": "Flight details for NERC-ARF aircraft flight number 2018_135a. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2748, "bboxName": "", "eastBoundLongitude": 1.1473148644735627, "westBoundLongitude": 0.9958475795040317, "southBoundLatitude": 52.09342930501146, "northBoundLatitude": 52.132280748683016 }, "operationTime": { "ob_id": 8912, "startTime": "2018-05-15T11:43:21", "endTime": "2018-05-15T12:00:36" }, "childOperation": null }, { "ob_id": 32451, "uuid": "795d66fa3fcf40f9a3c170496c5ec499", "short_code": "mpop", "title": "NERC-ARF flight 2018_135b", "abstract": "Flight details for NERC-ARF aircraft flight number 2018_135b. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2750, "bboxName": "", "eastBoundLongitude": -0.747077943142916, "westBoundLongitude": -0.8394999872174435, "southBoundLatitude": 53.34176255807064, "northBoundLatitude": 53.43532662810588 }, "operationTime": { "ob_id": 8914, "startTime": "2018-05-15T13:02:30", "endTime": "2018-05-15T13:37:51" }, "childOperation": null }, { "ob_id": 32476, "uuid": "6b0c1a7351894939bba41cace64139ff", "short_code": "mpop", "title": "NERC-ARF flight 292", "abstract": "Flight details for NERC-ARF aircraft flight number 292. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2753, "bboxName": "", "eastBoundLongitude": -18.069944381713867, "westBoundLongitude": -21.882347106933594, "southBoundLatitude": 65.64600372314453, "northBoundLatitude": 69.43681335449219 }, "operationTime": { "ob_id": 8919, "startTime": "2018-02-28T07:34:09", "endTime": "2018-02-28T11:51:10" }, "childOperation": null }, { "ob_id": 32481, "uuid": "6a1d6176610b40af8bf34fb4c96495e6", "short_code": "mpop", "title": "NERC-ARF flight 293", "abstract": "Flight details for NERC-ARF aircraft flight number 293. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2754, "bboxName": "", "eastBoundLongitude": -17.456592559814453, "westBoundLongitude": -22.173479080200195, "southBoundLatitude": 65.64640808105469, "northBoundLatitude": 70.47631072998047 }, "operationTime": { "ob_id": 8920, "startTime": "2018-03-01T08:02:05", "endTime": "2018-03-01T11:45:16" }, "childOperation": null }, { "ob_id": 32485, "uuid": "8352e6a2bf054fe48b79b96981b808d5", "short_code": "mpop", "title": "NERC-ARF flight 294", "abstract": "Flight details for NERC-ARF aircraft flight number 294. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2755, "bboxName": "", "eastBoundLongitude": -15.936248779296875, "westBoundLongitude": -22.6532039642334, "southBoundLatitude": 66.00090026855469, "northBoundLatitude": 70.74533081054688 }, "operationTime": { "ob_id": 8921, "startTime": "2018-03-01T12:59:15", "endTime": "2018-03-01T18:02:03" }, "childOperation": null }, { "ob_id": 32534, "uuid": "cdef402fe8404fae81d9d5d2209113fc", "short_code": "mpop", "title": "NERC-ARF flight 295", "abstract": "Flight details for NERC-ARF aircraft flight number 295. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2763, "bboxName": "", "eastBoundLongitude": -16.833900451660156, "westBoundLongitude": -19.00248908996582, "southBoundLatitude": 65.64497375488281, "northBoundLatitude": 70.31584167480469 }, "operationTime": { "ob_id": 8930, "startTime": "2018-03-04T10:08:36", "endTime": "2018-03-04T15:09:02" }, "childOperation": null }, { "ob_id": 32538, "uuid": "9381690c5d984b6e8005e7446393bef9", "short_code": "mpop", "title": "NERC-ARF flight 296", "abstract": "Flight details for NERC-ARF aircraft flight number 296. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. 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See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. 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See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. 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See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2767, "bboxName": "", "eastBoundLongitude": -18.334707260131836, "westBoundLongitude": -24.013635635375977, "southBoundLatitude": 65.41260528564453, "northBoundLatitude": 70.74539184570312 }, "operationTime": { "ob_id": 8934, "startTime": "2018-03-08T13:22:36", "endTime": "2018-03-08T19:01:49" }, "childOperation": null }, { "ob_id": 32554, "uuid": "df30e19bd3a84bd7a1506e3500bfe75b", "short_code": "mpop", "title": "NERC-ARF flight 300", "abstract": "Flight details for NERC-ARF aircraft flight number 300. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2768, "bboxName": "", "eastBoundLongitude": -18.084840774536133, "westBoundLongitude": -23.36092185974121, "southBoundLatitude": 65.72164154052734, "northBoundLatitude": 69.23255157470703 }, "operationTime": { "ob_id": 8935, "startTime": "2018-03-09T09:58:22", "endTime": "2018-03-09T14:47:07" }, "childOperation": null }, { "ob_id": 32558, "uuid": "0f9ac595a64a4dc89accd2b78a62f328", "short_code": "mpop", "title": "NERC-ARF flight 301", "abstract": "Flight details for NERC-ARF aircraft flight number 301. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2769, "bboxName": "", "eastBoundLongitude": -18.06656265258789, "westBoundLongitude": -24.609283447265625, "southBoundLatitude": 64.1262435913086, "northBoundLatitude": 65.6668701171875 }, "operationTime": { "ob_id": 8936, "startTime": "2018-03-12T12:04:34", "endTime": "2018-03-12T18:13:35" }, "childOperation": null }, { "ob_id": 32562, "uuid": "e4c4926dd3164e0cb1b5e47ccb0ae6ba", "short_code": "mpop", "title": "NERC-ARF flight 306", "abstract": "Flight details for NERC-ARF aircraft flight number 306. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. 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Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2770, "bboxName": "", "eastBoundLongitude": -18.050004959106445, "westBoundLongitude": -22.62369728088379, "southBoundLatitude": 65.63907623291016, "northBoundLatitude": 66.79524993896484 }, "operationTime": { "ob_id": 8937, "startTime": "2018-03-19T12:58:18", "endTime": "2018-03-19T17:29:32" }, "childOperation": null }, { "ob_id": 32566, "uuid": "1a4493b019e34bd89abd95f181e4235f", "short_code": "mpop", "title": "NERC-ARF flight 303", "abstract": "Flight details for NERC-ARF aircraft flight number 303. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2771, "bboxName": "", "eastBoundLongitude": -18.249908447265625, "westBoundLongitude": -22.6533203125, "southBoundLatitude": 66.03550720214844, "northBoundLatitude": 71.8899917602539 }, "operationTime": { "ob_id": 8938, "startTime": "2018-03-14T12:54:06", "endTime": "2018-03-14T18:28:13" }, "childOperation": null }, { "ob_id": 32570, "uuid": "1146d448ac0140b1aa230f03bc77e2be", "short_code": "mpop", "title": "NERC-ARF flight 304", "abstract": "Flight details for NERC-ARF aircraft flight number 304. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2772, "bboxName": "", "eastBoundLongitude": -16.815567016601562, "westBoundLongitude": -18.355791091918945, "southBoundLatitude": 65.64727020263672, "northBoundLatitude": 66.24910736083984 }, "operationTime": { "ob_id": 8939, "startTime": "2018-03-16T09:41:15", "endTime": "2018-03-16T11:45:26" }, "childOperation": null }, { "ob_id": 32574, "uuid": "bccead31fc3e429796e8e51d0feb0345", "short_code": "mpop", "title": "NERC-ARF flight 305", "abstract": "Flight details for NERC-ARF aircraft flight number 305. See linked documentation for further details.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2773, "bboxName": "", "eastBoundLongitude": -7.92543888092041, "westBoundLongitude": -18.19221305847168, "southBoundLatitude": 65.64600372314453, "northBoundLatitude": 70.66168212890625 }, "operationTime": { "ob_id": 8940, "startTime": "2018-03-18T09:00:10", "endTime": "2018-03-18T14:59:32" }, "childOperation": null }, { "ob_id": 33280, "uuid": "68254e57333b4fb988d122d15ada9703", "short_code": "mpop", "title": "MRF Flight C-130 A257", "abstract": "MRF Flight C-130 A257", "status": "completed", "platform_field": { "ob_id": 434, "uuid": "f1971a20238b4f5bba4126996bd2816d", "short_code": "plat", "title": "Met Office C-130 Hercules Aircraft", "abstract": "From 1972 to 2001 the Meteorological Research Flight (MRF) operated a C-130 aircraft which was comprehensively equipped to make a wide variety of atmospheric observations. It had been heavily modified for this role and was one of the most sophisticated 'flying laboratories' for atmospheric research in the world. The long striped probe on the nose allows sensitive instruments to make measurements, for example of turbulence, in a region outside the influence of the aircraft itself; it also gives the aircraft its nickname of 'Snoopy'." }, "location": { "ob_id": 2876, "bboxName": "a257 flight", "eastBoundLongitude": -0.7777, "westBoundLongitude": -3.08724, "southBoundLatitude": 51.28335, "northBoundLatitude": 58.45334 }, "operationTime": { "ob_id": 9141, "startTime": "1993-05-27T10:05:05", "endTime": "1993-05-27T16:17:03" }, "childOperation": null }, { "ob_id": 34781, "uuid": "d29f557a318d47a5b630c7a9a6ed9399", "short_code": "mpop", "title": "BAS-MASIN flight 319", "abstract": "Flight details for BAS-MASIN flight number 319.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2957, "bboxName": "", "eastBoundLongitude": -58.1330451965332, "westBoundLongitude": -60.19420623779297, "southBoundLatitude": -53.48469543457031, "northBoundLatitude": -51.81715774536133 }, "operationTime": { "ob_id": 9637, "startTime": "2019-02-23T12:28:49", "endTime": "2019-02-23T15:53:11" }, "childOperation": null }, { "ob_id": 34785, "uuid": "66e18ad79af749f98dd16cb68de369c2", "short_code": "mpop", "title": "BAS-MASIN flight 276", "abstract": "Flight details for BAS-MASIN flight number 276.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2958, "bboxName": "", "eastBoundLongitude": -68.1233139038086, "westBoundLongitude": -72.52396392822266, "southBoundLatitude": -68.09053039550781, "northBoundLatitude": -66.77977752685547 }, "operationTime": { "ob_id": 9638, "startTime": "2017-12-02T17:48:43", "endTime": "2017-12-02T21:42:41" }, "childOperation": null }, { "ob_id": 34789, "uuid": "6f6bce6856bf4255a402e3eaafed7fa0", "short_code": "mpop", "title": "BAS-MASIN flight 277", "abstract": "Flight details for BAS-MASIN flight number 277.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2959, "bboxName": "", "eastBoundLongitude": -60.03062057495117, "westBoundLongitude": -68.1306381225586, "southBoundLatitude": -68.24311065673828, "northBoundLatitude": -66.55838775634766 }, "operationTime": { "ob_id": 9639, "startTime": "2017-12-03T15:13:37", "endTime": "2017-12-03T20:09:20" }, "childOperation": null }, { "ob_id": 34793, "uuid": "b141bf08c8374c009d1d4cc4e8415177", "short_code": "mpop", "title": "BAS-MASIN flight 278", "abstract": "Flight details for BAS-MASIN flight number 278.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2960, "bboxName": "", "eastBoundLongitude": -58.763240814208984, "westBoundLongitude": -67.82427978515625, "southBoundLatitude": -67.43220520019531, "northBoundLatitude": -62.15033721923828 }, "operationTime": { "ob_id": 9640, "startTime": "2017-12-06T14:21:54", "endTime": "2017-12-06T17:07:43" }, "childOperation": null }, { "ob_id": 34797, "uuid": "1f40ad5ce5f948cfa7404ad878d0c585", "short_code": "mpop", "title": "BAS-MASIN flight 279", "abstract": "Flight details for BAS-MASIN flight number 279.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2961, "bboxName": "", "eastBoundLongitude": -58.984230041503906, "westBoundLongitude": -65.77291870117188, "southBoundLatitude": -62.19147491455078, "northBoundLatitude": -61.17997741699219 }, "operationTime": { "ob_id": 9641, "startTime": "2017-12-06T19:09:32", "endTime": "2017-12-06T22:45:59" }, "childOperation": null }, { "ob_id": 34801, "uuid": "0d812553e9c74e0ab5d38b12d1b87c97", "short_code": "mpop", "title": "BAS-MASIN flight 289", "abstract": "Flight details for BAS-MASIN flight number 289.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2962, "bboxName": "", "eastBoundLongitude": -67.86925506591797, "westBoundLongitude": -71.6224136352539, "southBoundLatitude": -68.78662109375, "northBoundLatitude": -67.55120849609375 }, "operationTime": { "ob_id": 9642, "startTime": "2017-12-16T13:03:51", "endTime": "2017-12-16T17:08:52" }, "childOperation": null }, { "ob_id": 34805, "uuid": "c25881869fa34362a9a65386b850cbb8", "short_code": "mpop", "title": "BAS-MASIN flight 280", "abstract": "Flight details for BAS-MASIN flight number 280.", "status": "completed", "platform_field": { "ob_id": 7575, "uuid": "2a863d6731c44af2aedda1da73e1015b", "short_code": "plat", "title": "BAS Twin-Otter aircraft", "abstract": "The British Antarctic Survey has a Twin Otter aircraft with a certified fit of airborne atmospheric instrumentation suitable for atmospheric, boundary layer and cloud/aerosol studies.\r\n\r\nThe Twin Otter aircraft is a very adaptable platform used the world over as a ‘bush’ aircraft. Its twin turbo-prop engines and ‘Short Take off and Landing’ (STOL) capability allow it to be used from small, remote unpaved airfields and the addition of skis or tundra tyres also allows operation on snow and from remote camps.\r\n\r\nThe aircraft can be operated single pilot and a long range fuel tank is also available. Double cargo doors provide good access for installing instrument racks.\r\n\r\nIn general the aircraft works in the Antarctic from October through to March each year depending on projects, and can operate at other latitudes outside this period, for example ACCACIA in the Arctic February 2013.\r\n\r\nThe instrument suite includes standard temperature and water vapour sensors as well as a turbulence probe allowing full atmospheric profile measurements of temperature, dew point and winds.\r\n\r\nThe fast turbulence probe also facilitates sensible heat flux measurements by the eddy covariance method. These boundary layer measurement capabilities are complemented by incoming and outgoing radiation instruments and a downward looking infra-red thermometer.\r\n\r\nThe floor hatch opening can also accommodate a fixed laser range finder or scanning laser which has been used for measuring ice floe topography. The required GPS and attitude measurements to support this are available. Video and digital SLR cameras can also be fitted here. The camera bay can also be configured to drop airborne deployable buoys.\r\n\r\nHard points and pylons are available on each wing. A DMT Cloud and aerosol spectrometer (CAPS) probe is used for cloud studies. Other standard PMS pod instruments can easily be accommodated. A closed path Licor H2O/CO2 instrument, Grimm optical particle counter and cloud condensation nuclei counter are fed from simple Rosemount inlets.\r\n\r\nRange:\t1000km including skis. Increased with long range tank depending on configuration.\r\nAirspeed:\tCruise 65m/s. Data collection 60m/s.\r\nComplement:\tPilot + maximum 4 mission operators / scientists.\r\nAltitudes:\tless than 35m to 5000m. Unpressurized but with oxygen fit for pilots and operators." }, "location": { "ob_id": 2963, "bboxName": "", "eastBoundLongitude": -58.97597885131836, "westBoundLongitude": -67.92103576660156, "southBoundLatitude": -67.43942260742188, "northBoundLatitude": -62.14649963378906 }, "operationTime": { "ob_id": 9643, "startTime": "2017-12-07T12:26:36", "endTime": "2017-12-07T15:52:58" }, "childOperation": null } ] }