Instrument Platform Pair List

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    "results": [
        {
            "ob_id": 12339,
            "platform": {
                "ob_id": 6687,
                "uuid": "4fc04d0f05ea4619845f04aed761e540",
                "short_code": "plat",
                "title": "Centre for Ecology and Hydrology (CEH) Auchencorth Moss field site",
                "abstract": "The Auchencorth Moss site, located in an elevated rural environment, 1.5 kilometres north west of the A701 at Leadburn and 18 kilometres south of Edinburgh city centre, Scotland, near Penicuik. It has been operational since 1985 as part of a variety of different monitoring networks, including being one of two two Level III 'supersites' located in the UK of the EMEP (the Co-operative Programme for Monitoring and Evaluation of the Long-range Transmission of Air Pollutants in Europe) monitoring network. Hourly and daily measurements are supplemented by long-term integrated measurements from existing DEFRA-funded monitoring networks across the UK (http://www.nilu.no/projects/ccc/network/index.html) Auchencorth Moss is the northern of these two sites (the other is near Harwell, Oxfordshire), which has been used by the Centre for Ecology & Hydrology for several years as an intensive monitoring site for trace gas and particle concentrations and fluxes. The site is based in an area of upland deep peat, with heather and grass cover, and has an extensive fetch to the south-west. The site is located at 55.792160 N, 3.242900W (OS Grid map reference: NT 322166, 656128) and at an altitude of 260m above mean sea level. The site is mostly funded by DEFRA but with significant CEH support, part-funded by EU ACTRIS Programme. The CEH field team carry out routine monitoring work for DEFRA and other funding agency contracts. Intermittent research activities are carried out by scientists both from CEH and other UK and international organisations. As a result of the large number of parameter measured at the site it is part of a wide range of monitoring networks. For details of these networks visit the DEFRA station details page. Details of individual activities should be found either on relevant databases (including the BADC) or by contacting CEH for further information. The station's UK-AIR ID is UKA00451 and its EU Site ID (EMEP network identifier) is GB0048R."
            },
            "instrument": {
                "ob_id": 30615,
                "uuid": "2ab86dc13efb42c192b4b1942f02cd0b",
                "short_code": "instr",
                "title": "UK Centre for Ecology & Hydrology j(NO2) 4-pi filter radiometer",
                "abstract": "Measured broadband j(NO2) photolysis rate constants from down- and upwelling directions at Auchencorth Moss."
            },
            "relatedTo": {
                "ob_id": 30614,
                "uuid": "e9d23ef7634d469a87b25297a88ea3d5",
                "short_code": "acq",
                "title": "Acquisition for: Hourly averaged 4-pi filter radiometer measurements at Auchencorth Moss (21/11/2018 - 20/11/2019) near Edinburgh (UK)",
                "abstract": "Acquisition for: Hourly averaged 4-pi filter radiometer measurements at Auchencorth Moss (21/11/2018 - 20/11/2019) near Edinburgh (UK)"
            }
        },
        {
            "ob_id": 12340,
            "platform": {
                "ob_id": 12460,
                "uuid": "d716b34f2dee47128e93691f70b8dff0",
                "short_code": "plat",
                "title": "Met Office Weather Station, Camborne, UK",
                "abstract": "The Met Office operate a weather station (WMO id 03808) near Camborne, Cornwall, located 87m above mean sea level in Cornwall, south-west UK. Since 1978 meteorological observations have been recorded on a 24 hr basis, linking the station to the synoptic network of the Met Office Meteorological Service. The site is located at OS grid reference SW 627406 . More information can be found in the linked documents. Upper air observations from the site have also been made via ceilometer, radiosonde and boundary-layer wind profiler."
            },
            "instrument": {
                "ob_id": 26255,
                "uuid": "e9c0a99af62c4506b2af5da7c75c82b2",
                "short_code": "instr",
                "title": "Met Office: Raymetrics LR111-D300 Raman lidar",
                "abstract": "The Met Office operate a network of 10 Raymetrics LR111-D300 Raman lidars as part of their aerosol remote sensing capability. The network consists of nine fixed locations evenly distributed across Britain, and one mobile facility normally located at Watnall near Nottingham (Adam et al. 2017). The first lidar was installed at the Camborne site in 2015, and the network was fully installed by September 2016. The lidars, Raymetrics LR111-300s, are bespoke systems developed and manufactured by Raymetrics to meet the Met Office and London Volcanic Ash Advisory Centre (VAAC) needs. The instruments emit at 355nm and have polar and co-polar depolarisation detection channels at 355nm, and an N2 Raman detection channel at 387nm. The polarization channels of each lidar are calibrated using the + / - 45 degree procedure from Freudenthaler et al. 2009. Alignment is ensured using the telecover test described in Freudenthaler et al. 2018. Co-located with the lidars are Cimel CE318 multiband sun-photometers, which are part of the AERONET network. Each lidar is operated remotely from the Met Office Exeter headquarters. The primary aim of the network is the detection and quantification of volcanic ash aerosols during a volcanic event, and the network is only test fired only for a few hours each week. Outside of these times the lidars may be fired if there is a mineral dust outbreak or other such aerosol event of interest. The lidars will not fire if any precipitation is detected.\r\n\r\nTransmitter: Quantel CFR200 laser at 355nm, with 50mJ/pulse at 20Hz (i.e. 1W) and is \"eye-safe\"\r\nReceiver: 30cm diameter telescope\r\nDetectors for 355nm (parallel and perpendicular polarization) and 387nm (N2 Raman channel)\r\nBeam and receiving telescope's field of view having complete overlap at ~250m.\r\nLidar beam has a near-vertically pointing direction.\r\n\r\nAdam, M., Buxmann, J., Freeman, N., Horseman, A., Slamon, C., Sugier, J., and Bennett, R.: The UK Lidar-Sunphotometer Operational Volcanic Ash Monitoring Network, in: Proceedings of the 28th International Laser Radar Conference, 2017.\r\n\r\nFreudenthaler, V., Esselborne, M., Wiegner, M., Heese, B., Tesche, M., Ansmann, A., Muller, D., Althausen, D., Wirth, M., Fix, A., Ehret, G., Knippertz, P., Toledano, C., Gasteiger, J., Garhammer, M., and Seefeldner, M.: Depolarization ratio profiling at several wavelengths in pure Saharan dust during SAMUM 2006, Tellus B, 61, 165-179, http://dx.doi.org/10.1111/j.1600-0889.2008.00396.x, 2009.\r\n\r\nFreudenthaler, V., Linné, H., Chaikovski, A., Rabus, D., and Groß, S.: EARLINET lidar quality assurance tools, Atmospheric Measurement Techniques Discussions, 2018, 1-35, https://doi.org/10.5194/amt-2017-395, https://www.atmos-meas-tech-discuss.net/amt-2017-395/, 2018."
            },
            "relatedTo": {
                "ob_id": 31557,
                "uuid": "6100059eaf5a47af89137321b903ba9e",
                "short_code": "acq",
                "title": "Acquisition for Met Office Raman Lidar obs for ex hurricane Ophelia",
                "abstract": "Acquisition for Met Office Raman Lidar obs for ex hurricane Ophelia"
            }
        },
        {
            "ob_id": 12341,
            "platform": {
                "ob_id": 1012,
                "uuid": "358641354ff546c2a761c9094c414373",
                "short_code": "plat",
                "title": "Met Office Nottingham Watnall site, UK",
                "abstract": "The Met Office operate an observation site at Nottingham Watnall (WMO id 03354) hosting a suite of instruments including surface meteorological observations, laser ceilometer and has been used for radiosonde launches.  The station is located 117m above mean sea level in Nottinghamshire, east UK. Since 1941 meteorological observations have been recorded on a 24hr basis, linking the station to the synoptic network of the Met Office Meteorological Service. The site is located at OS grid reference SK 503456. More information can be found in the linked documents.\n\nSite WIGOS id: 0-20000-0-03354. See online documentation for link to station details in the Observing Systems Capability Analysis and Review (OSCAR) Tool."
            },
            "instrument": {
                "ob_id": 26255,
                "uuid": "e9c0a99af62c4506b2af5da7c75c82b2",
                "short_code": "instr",
                "title": "Met Office: Raymetrics LR111-D300 Raman lidar",
                "abstract": "The Met Office operate a network of 10 Raymetrics LR111-D300 Raman lidars as part of their aerosol remote sensing capability. The network consists of nine fixed locations evenly distributed across Britain, and one mobile facility normally located at Watnall near Nottingham (Adam et al. 2017). The first lidar was installed at the Camborne site in 2015, and the network was fully installed by September 2016. The lidars, Raymetrics LR111-300s, are bespoke systems developed and manufactured by Raymetrics to meet the Met Office and London Volcanic Ash Advisory Centre (VAAC) needs. The instruments emit at 355nm and have polar and co-polar depolarisation detection channels at 355nm, and an N2 Raman detection channel at 387nm. The polarization channels of each lidar are calibrated using the + / - 45 degree procedure from Freudenthaler et al. 2009. Alignment is ensured using the telecover test described in Freudenthaler et al. 2018. Co-located with the lidars are Cimel CE318 multiband sun-photometers, which are part of the AERONET network. Each lidar is operated remotely from the Met Office Exeter headquarters. The primary aim of the network is the detection and quantification of volcanic ash aerosols during a volcanic event, and the network is only test fired only for a few hours each week. Outside of these times the lidars may be fired if there is a mineral dust outbreak or other such aerosol event of interest. The lidars will not fire if any precipitation is detected.\r\n\r\nTransmitter: Quantel CFR200 laser at 355nm, with 50mJ/pulse at 20Hz (i.e. 1W) and is \"eye-safe\"\r\nReceiver: 30cm diameter telescope\r\nDetectors for 355nm (parallel and perpendicular polarization) and 387nm (N2 Raman channel)\r\nBeam and receiving telescope's field of view having complete overlap at ~250m.\r\nLidar beam has a near-vertically pointing direction.\r\n\r\nAdam, M., Buxmann, J., Freeman, N., Horseman, A., Slamon, C., Sugier, J., and Bennett, R.: The UK Lidar-Sunphotometer Operational Volcanic Ash Monitoring Network, in: Proceedings of the 28th International Laser Radar Conference, 2017.\r\n\r\nFreudenthaler, V., Esselborne, M., Wiegner, M., Heese, B., Tesche, M., Ansmann, A., Muller, D., Althausen, D., Wirth, M., Fix, A., Ehret, G., Knippertz, P., Toledano, C., Gasteiger, J., Garhammer, M., and Seefeldner, M.: Depolarization ratio profiling at several wavelengths in pure Saharan dust during SAMUM 2006, Tellus B, 61, 165-179, http://dx.doi.org/10.1111/j.1600-0889.2008.00396.x, 2009.\r\n\r\nFreudenthaler, V., Linné, H., Chaikovski, A., Rabus, D., and Groß, S.: EARLINET lidar quality assurance tools, Atmospheric Measurement Techniques Discussions, 2018, 1-35, https://doi.org/10.5194/amt-2017-395, https://www.atmos-meas-tech-discuss.net/amt-2017-395/, 2018."
            },
            "relatedTo": {
                "ob_id": 31557,
                "uuid": "6100059eaf5a47af89137321b903ba9e",
                "short_code": "acq",
                "title": "Acquisition for Met Office Raman Lidar obs for ex hurricane Ophelia",
                "abstract": "Acquisition for Met Office Raman Lidar obs for ex hurricane Ophelia"
            }
        },
        {
            "ob_id": 12342,
            "platform": {
                "ob_id": 26271,
                "uuid": "1d9c08e8afc04876bd85671c48fc7658",
                "short_code": "plat",
                "title": "Met Office Loftus Meteorological Station",
                "abstract": "The Met Office Loftus Meteorological Station (WMO ID: 03275), located in North Yorkshire, has been operated since 1996. The site supports surface and upper air meteorological observations, including Raman lidar operations. It is located 158 m above MSL and has been operational since 1996."
            },
            "instrument": {
                "ob_id": 26255,
                "uuid": "e9c0a99af62c4506b2af5da7c75c82b2",
                "short_code": "instr",
                "title": "Met Office: Raymetrics LR111-D300 Raman lidar",
                "abstract": "The Met Office operate a network of 10 Raymetrics LR111-D300 Raman lidars as part of their aerosol remote sensing capability. The network consists of nine fixed locations evenly distributed across Britain, and one mobile facility normally located at Watnall near Nottingham (Adam et al. 2017). The first lidar was installed at the Camborne site in 2015, and the network was fully installed by September 2016. The lidars, Raymetrics LR111-300s, are bespoke systems developed and manufactured by Raymetrics to meet the Met Office and London Volcanic Ash Advisory Centre (VAAC) needs. The instruments emit at 355nm and have polar and co-polar depolarisation detection channels at 355nm, and an N2 Raman detection channel at 387nm. The polarization channels of each lidar are calibrated using the + / - 45 degree procedure from Freudenthaler et al. 2009. Alignment is ensured using the telecover test described in Freudenthaler et al. 2018. Co-located with the lidars are Cimel CE318 multiband sun-photometers, which are part of the AERONET network. Each lidar is operated remotely from the Met Office Exeter headquarters. The primary aim of the network is the detection and quantification of volcanic ash aerosols during a volcanic event, and the network is only test fired only for a few hours each week. Outside of these times the lidars may be fired if there is a mineral dust outbreak or other such aerosol event of interest. The lidars will not fire if any precipitation is detected.\r\n\r\nTransmitter: Quantel CFR200 laser at 355nm, with 50mJ/pulse at 20Hz (i.e. 1W) and is \"eye-safe\"\r\nReceiver: 30cm diameter telescope\r\nDetectors for 355nm (parallel and perpendicular polarization) and 387nm (N2 Raman channel)\r\nBeam and receiving telescope's field of view having complete overlap at ~250m.\r\nLidar beam has a near-vertically pointing direction.\r\n\r\nAdam, M., Buxmann, J., Freeman, N., Horseman, A., Slamon, C., Sugier, J., and Bennett, R.: The UK Lidar-Sunphotometer Operational Volcanic Ash Monitoring Network, in: Proceedings of the 28th International Laser Radar Conference, 2017.\r\n\r\nFreudenthaler, V., Esselborne, M., Wiegner, M., Heese, B., Tesche, M., Ansmann, A., Muller, D., Althausen, D., Wirth, M., Fix, A., Ehret, G., Knippertz, P., Toledano, C., Gasteiger, J., Garhammer, M., and Seefeldner, M.: Depolarization ratio profiling at several wavelengths in pure Saharan dust during SAMUM 2006, Tellus B, 61, 165-179, http://dx.doi.org/10.1111/j.1600-0889.2008.00396.x, 2009.\r\n\r\nFreudenthaler, V., Linné, H., Chaikovski, A., Rabus, D., and Groß, S.: EARLINET lidar quality assurance tools, Atmospheric Measurement Techniques Discussions, 2018, 1-35, https://doi.org/10.5194/amt-2017-395, https://www.atmos-meas-tech-discuss.net/amt-2017-395/, 2018."
            },
            "relatedTo": {
                "ob_id": 31557,
                "uuid": "6100059eaf5a47af89137321b903ba9e",
                "short_code": "acq",
                "title": "Acquisition for Met Office Raman Lidar obs for ex hurricane Ophelia",
                "abstract": "Acquisition for Met Office Raman Lidar obs for ex hurricane Ophelia"
            }
        },
        {
            "ob_id": 12343,
            "platform": {
                "ob_id": 26273,
                "uuid": "01b48516da934109a808906cd0ba14dc",
                "short_code": "plat",
                "title": "Met Office Rhyl Meteorological Station",
                "abstract": "The Met Office Rhyl Meteorological Station (WMO ID: 03313) is an instrument enclosure located near Rhyl, North Wales, and has been operated since 1986. The site supports surface and upper air meteorological observations, including Raman lidar operations. It is located 77 m above MSL."
            },
            "instrument": {
                "ob_id": 26255,
                "uuid": "e9c0a99af62c4506b2af5da7c75c82b2",
                "short_code": "instr",
                "title": "Met Office: Raymetrics LR111-D300 Raman lidar",
                "abstract": "The Met Office operate a network of 10 Raymetrics LR111-D300 Raman lidars as part of their aerosol remote sensing capability. The network consists of nine fixed locations evenly distributed across Britain, and one mobile facility normally located at Watnall near Nottingham (Adam et al. 2017). The first lidar was installed at the Camborne site in 2015, and the network was fully installed by September 2016. The lidars, Raymetrics LR111-300s, are bespoke systems developed and manufactured by Raymetrics to meet the Met Office and London Volcanic Ash Advisory Centre (VAAC) needs. The instruments emit at 355nm and have polar and co-polar depolarisation detection channels at 355nm, and an N2 Raman detection channel at 387nm. The polarization channels of each lidar are calibrated using the + / - 45 degree procedure from Freudenthaler et al. 2009. Alignment is ensured using the telecover test described in Freudenthaler et al. 2018. Co-located with the lidars are Cimel CE318 multiband sun-photometers, which are part of the AERONET network. Each lidar is operated remotely from the Met Office Exeter headquarters. The primary aim of the network is the detection and quantification of volcanic ash aerosols during a volcanic event, and the network is only test fired only for a few hours each week. Outside of these times the lidars may be fired if there is a mineral dust outbreak or other such aerosol event of interest. The lidars will not fire if any precipitation is detected.\r\n\r\nTransmitter: Quantel CFR200 laser at 355nm, with 50mJ/pulse at 20Hz (i.e. 1W) and is \"eye-safe\"\r\nReceiver: 30cm diameter telescope\r\nDetectors for 355nm (parallel and perpendicular polarization) and 387nm (N2 Raman channel)\r\nBeam and receiving telescope's field of view having complete overlap at ~250m.\r\nLidar beam has a near-vertically pointing direction.\r\n\r\nAdam, M., Buxmann, J., Freeman, N., Horseman, A., Slamon, C., Sugier, J., and Bennett, R.: The UK Lidar-Sunphotometer Operational Volcanic Ash Monitoring Network, in: Proceedings of the 28th International Laser Radar Conference, 2017.\r\n\r\nFreudenthaler, V., Esselborne, M., Wiegner, M., Heese, B., Tesche, M., Ansmann, A., Muller, D., Althausen, D., Wirth, M., Fix, A., Ehret, G., Knippertz, P., Toledano, C., Gasteiger, J., Garhammer, M., and Seefeldner, M.: Depolarization ratio profiling at several wavelengths in pure Saharan dust during SAMUM 2006, Tellus B, 61, 165-179, http://dx.doi.org/10.1111/j.1600-0889.2008.00396.x, 2009.\r\n\r\nFreudenthaler, V., Linné, H., Chaikovski, A., Rabus, D., and Groß, S.: EARLINET lidar quality assurance tools, Atmospheric Measurement Techniques Discussions, 2018, 1-35, https://doi.org/10.5194/amt-2017-395, https://www.atmos-meas-tech-discuss.net/amt-2017-395/, 2018."
            },
            "relatedTo": {
                "ob_id": 31557,
                "uuid": "6100059eaf5a47af89137321b903ba9e",
                "short_code": "acq",
                "title": "Acquisition for Met Office Raman Lidar obs for ex hurricane Ophelia",
                "abstract": "Acquisition for Met Office Raman Lidar obs for ex hurricane Ophelia"
            }
        },
        {
            "ob_id": 12344,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31639,
                "uuid": "8373da9c8a9d40eba2d9ce0b68f57319",
                "short_code": "acq",
                "title": "Acquisition for: ARSF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12345,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31643,
                "uuid": "a32997f5920a4b2b9f7ed78e6f05a88f",
                "short_code": "acq",
                "title": "Acquisition for: ARSF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12346,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31643,
                "uuid": "a32997f5920a4b2b9f7ed78e6f05a88f",
                "short_code": "acq",
                "title": "Acquisition for: ARSF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12347,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31643,
                "uuid": "a32997f5920a4b2b9f7ed78e6f05a88f",
                "short_code": "acq",
                "title": "Acquisition for: ARSF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12348,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24845,
                "uuid": "4f82e9e3c71140d499e7dbbe5d50da00",
                "short_code": "instr",
                "title": "NERC-ARF Specim AISA Owl",
                "abstract": "The Specim AISAOwl is a hyperspectral imager on board the NERC-ARF aircraft measuring the Long Wave InfraRed (LWIR) wavelengths, specifically 7.5–12.5 um with 102 bands. It is a passive pushbroom sensor measuring primarily emitted radiation, which can be used to derive temperature and emissivity."
            },
            "relatedTo": {
                "ob_id": 31643,
                "uuid": "a32997f5920a4b2b9f7ed78e6f05a88f",
                "short_code": "acq",
                "title": "Acquisition for: ARSF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12349,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31653,
                "uuid": "6b8d7b7a813b4fa4bd3a323160e1e86f",
                "short_code": "acq",
                "title": "Acquisition for: ARSF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12350,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31653,
                "uuid": "6b8d7b7a813b4fa4bd3a323160e1e86f",
                "short_code": "acq",
                "title": "Acquisition for: ARSF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12351,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31653,
                "uuid": "6b8d7b7a813b4fa4bd3a323160e1e86f",
                "short_code": "acq",
                "title": "Acquisition for: ARSF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12352,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24845,
                "uuid": "4f82e9e3c71140d499e7dbbe5d50da00",
                "short_code": "instr",
                "title": "NERC-ARF Specim AISA Owl",
                "abstract": "The Specim AISAOwl is a hyperspectral imager on board the NERC-ARF aircraft measuring the Long Wave InfraRed (LWIR) wavelengths, specifically 7.5–12.5 um with 102 bands. It is a passive pushbroom sensor measuring primarily emitted radiation, which can be used to derive temperature and emissivity."
            },
            "relatedTo": {
                "ob_id": 31653,
                "uuid": "6b8d7b7a813b4fa4bd3a323160e1e86f",
                "short_code": "acq",
                "title": "Acquisition for: ARSF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12353,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31685,
                "uuid": "7cc6e4af022045a8ab5767c9fd0b8c18",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_293 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12354,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31685,
                "uuid": "7cc6e4af022045a8ab5767c9fd0b8c18",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_293 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12355,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31685,
                "uuid": "7cc6e4af022045a8ab5767c9fd0b8c18",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_293 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12356,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31689,
                "uuid": "e59eae62ecbb4f83a4254dfd84c51c12",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_291 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12357,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31689,
                "uuid": "e59eae62ecbb4f83a4254dfd84c51c12",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_291 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12358,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31689,
                "uuid": "e59eae62ecbb4f83a4254dfd84c51c12",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_291 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12359,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31693,
                "uuid": "bc09a3ffb11e4284a074321d78e6a037",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12360,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31693,
                "uuid": "bc09a3ffb11e4284a074321d78e6a037",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12361,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31693,
                "uuid": "bc09a3ffb11e4284a074321d78e6a037",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_290 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12362,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31697,
                "uuid": "b75d3b7dc5304f49a03c9ff2ac66271b",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_288 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12363,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31697,
                "uuid": "b75d3b7dc5304f49a03c9ff2ac66271b",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_288 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12364,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31697,
                "uuid": "b75d3b7dc5304f49a03c9ff2ac66271b",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_288 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12365,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31701,
                "uuid": "95b12a6fbeec40ed80c7b4cff467b542",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_289 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12366,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31701,
                "uuid": "95b12a6fbeec40ed80c7b4cff467b542",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_289 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12367,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31701,
                "uuid": "95b12a6fbeec40ed80c7b4cff467b542",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_289 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12368,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31705,
                "uuid": "d560a6eb4923426bb1be6665187247b9",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_294 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12369,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31705,
                "uuid": "d560a6eb4923426bb1be6665187247b9",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_294 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12370,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31705,
                "uuid": "d560a6eb4923426bb1be6665187247b9",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_294 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12371,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31709,
                "uuid": "2c132914f8f54657969acd129edbd983",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_295 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12372,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31709,
                "uuid": "2c132914f8f54657969acd129edbd983",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_295 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12373,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31709,
                "uuid": "2c132914f8f54657969acd129edbd983",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_295 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12374,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31713,
                "uuid": "0b00e5e79f024f669ff968d97a50a27e",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_297 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12375,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31713,
                "uuid": "0b00e5e79f024f669ff968d97a50a27e",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_297 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12376,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31713,
                "uuid": "0b00e5e79f024f669ff968d97a50a27e",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_297 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12377,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31717,
                "uuid": "bbde2bba402a48bf86a6fe7808616818",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_298 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12378,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31717,
                "uuid": "bbde2bba402a48bf86a6fe7808616818",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_298 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12379,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31717,
                "uuid": "bbde2bba402a48bf86a6fe7808616818",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_298 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12380,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31721,
                "uuid": "8ee9ac6e59574212b8e932b97af0d225",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_302a - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12381,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 31725,
                "uuid": "c61088a538a6461293bf606a57ea8f9e",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_303 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12382,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 20341,
                "uuid": "dc1c1ce7a82c4443b959edbf89c014d0",
                "short_code": "instr",
                "title": "NERC-ARF AsiaFENIX hyperspectral imager",
                "abstract": "The AisaFENIX dual sensor delivers high-quality hyperspectral data available in visible and SWIR wavelengths (380 - 2500nm) in a single continuous image. AisaFENIX eliminates past challenges in 'full spectrum imaging'. It is a single optics imager, with two focal plane arrays always staring exactly the same spot of the object. Thus, there is no need for the co-alignment of two separate imagers with different distortions, sharpness, and FOV.\r\n\r\nThe patent pending AisaFENIX images the target in 380 - 2500nm spectral region through single front optics and single input slit, keeping all wavebands spatially, co-registered, independent of the distance to the target. AisaFENIX employs Specim's patent pending 'single optics dual channel imaging spectrograph' which, in spite of the single input slit, has two diffraction gratings, one optimised for VNIR and the second for SWIR region. Also, two focal plane arrays (FPA), a state of the art CMOS and cryogenically cooled Mercury Telluride Cadmium (MCT), are employed in order to maximise sensitivity and signal-to-noise ratio (SNR) in the VNIR and SWIR spectral region.\r\n\r\nThe AsiaFENIX  is operated by NERC-ARF on board the British Antarctic Survey (BAS) Twin-Otter aircraft (Pre 2016 it was operated on board the NERC ARSF Dornier Do228-101 D-CALM Aircraft)"
            },
            "relatedTo": {
                "ob_id": 31725,
                "uuid": "c61088a538a6461293bf606a57ea8f9e",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_303 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12383,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 31725,
                "uuid": "c61088a538a6461293bf606a57ea8f9e",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_303 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12384,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24845,
                "uuid": "4f82e9e3c71140d499e7dbbe5d50da00",
                "short_code": "instr",
                "title": "NERC-ARF Specim AISA Owl",
                "abstract": "The Specim AISAOwl is a hyperspectral imager on board the NERC-ARF aircraft measuring the Long Wave InfraRed (LWIR) wavelengths, specifically 7.5–12.5 um with 102 bands. It is a passive pushbroom sensor measuring primarily emitted radiation, which can be used to derive temperature and emissivity."
            },
            "relatedTo": {
                "ob_id": 31725,
                "uuid": "c61088a538a6461293bf606a57ea8f9e",
                "short_code": "acq",
                "title": "Acquisition for: NERC-ARF 2014_303 - RG13_06 Flight: Airborne remote sensing measurements",
                "abstract": ""
            }
        },
        {
            "ob_id": 12385,
            "platform": {
                "ob_id": 30506,
                "uuid": "c58202085ddb493988be0fea4e1b065f",
                "short_code": "plat",
                "title": "Summit Station Greenland",
                "abstract": "The Summit Station in Greenland is located (72° 36’N, 38° 25’W, 3250m), atop the Greenland Ice Sheet making it a unique location for a cloud– atmosphere observatory. The station is about 400 km from the east and west coastlines and more than 1,000 km from the southwest and southeast coasts, from which most of the flow impinging on Summit originates, making it a distinctly continental environment. Additionally, the high altitude leads to extremely cold and dry conditions and a relative compression of the troposphere above the ice sheet."
            },
            "instrument": {
                "ob_id": 25986,
                "uuid": "e30e88421dde44ecb46f09736f289e5f",
                "short_code": "instr",
                "title": "University of Leeds: Licor Li-7500 gas analyzer",
                "abstract": "The University of Leeds' LI-COR LI-7500 open path gas analyser operates at infra-red wavelengths measuring the absorption due to carbon dioxide and water vapour concentrations at specific wavelengths along its 0.125m measurement path. Internally-stored calibration data are used to convert these absorption values to a mole concentration for each gas. Measurements are made at 20 Hz frequency."
            },
            "relatedTo": {
                "ob_id": 31767,
                "uuid": "f70c548dcb0148d4b459187280cdded1",
                "short_code": "acq",
                "title": "Acquisition for: ICECAPS-ACE: surface turbulent heat flux components",
                "abstract": "Acquisition for: ICECAPS-ACE: surface turbulent heat flux components"
            }
        },
        {
            "ob_id": 12386,
            "platform": {
                "ob_id": 26503,
                "uuid": "e494bef9ef884794a65a341e58205eb2",
                "short_code": "plat",
                "title": "Alliance Ship",
                "abstract": "Alliance  is a research ship. The 93 meters, 3,180 t NATO ship NRV ALLIANCE was designed in the mid 80’s as a quiet acoustic research platform. It is capable of operating in all oceans strategically important to NATO nations. ALLIANCE enables scientists and engineers from the Centre and partner nations to conduct a wide range of experiments. The ship is equipped with modern scientific instruments, a sophisticated navigation system, and its deck comprises of a vast array of winches (some fitted and some removable), heavy cranes, a lateral frame and a stern U-frame (including a large 4 drum main tow winch for large arrays). This variety of deck equipment allows a large variety of launch and recovery of scientific and engineering sensors, oceanographic instruments, autonomous vehicles and tethered devices."
            },
            "instrument": {
                "ob_id": 29986,
                "uuid": "8d7472c544e846c988cb49b3d2358eb9",
                "short_code": "instr",
                "title": "University of Bergen: Windcube lidar wind profiler",
                "abstract": "This is a lidar wind profiler built by leosphere and it belongs to and was operated by University of Bergen"
            },
            "relatedTo": {
                "ob_id": 31788,
                "uuid": "e0120de39d534374bfa65a6df64126a3",
                "short_code": "acq",
                "title": "Iceland Greenland Seas Project (IGP): surface layer meteorological measurements on board the NATO Research Vessel Alliance",
                "abstract": "Iceland Greenland Seas Project (IGP): surface layer meteorological measurements on board the NATO Research Vessel Alliance"
            }
        },
        {
            "ob_id": 12387,
            "platform": {
                "ob_id": 26503,
                "uuid": "e494bef9ef884794a65a341e58205eb2",
                "short_code": "plat",
                "title": "Alliance Ship",
                "abstract": "Alliance  is a research ship. The 93 meters, 3,180 t NATO ship NRV ALLIANCE was designed in the mid 80’s as a quiet acoustic research platform. It is capable of operating in all oceans strategically important to NATO nations. ALLIANCE enables scientists and engineers from the Centre and partner nations to conduct a wide range of experiments. The ship is equipped with modern scientific instruments, a sophisticated navigation system, and its deck comprises of a vast array of winches (some fitted and some removable), heavy cranes, a lateral frame and a stern U-frame (including a large 4 drum main tow winch for large arrays). This variety of deck equipment allows a large variety of launch and recovery of scientific and engineering sensors, oceanographic instruments, autonomous vehicles and tethered devices."
            },
            "instrument": {
                "ob_id": 26653,
                "uuid": "f93fa7f9725b406b899db743e9fb402a",
                "short_code": "instr",
                "title": "NCAS Scanning Radiometer- HATPRO",
                "abstract": "NCAS  Humidity And Temperature PROfiler (HATPRO) Scanning Microwave Radiometer unit 1, by Radiometer Physics GmbH. is used to derive vertical profiles of atmospheric temperature and humidity. The infrared radiometer extension allows to cloud base height and ice cloud detection.The radiometer offers high-resolution temperature profiling of the boundary layer and low-humidity applications. The radiometer provides accurate total amounts of atmospheric water vapor and cloud liquid content measurements."
            },
            "relatedTo": {
                "ob_id": 31788,
                "uuid": "e0120de39d534374bfa65a6df64126a3",
                "short_code": "acq",
                "title": "Iceland Greenland Seas Project (IGP): surface layer meteorological measurements on board the NATO Research Vessel Alliance",
                "abstract": "Iceland Greenland Seas Project (IGP): surface layer meteorological measurements on board the NATO Research Vessel Alliance"
            }
        },
        {
            "ob_id": 12388,
            "platform": {
                "ob_id": 26503,
                "uuid": "e494bef9ef884794a65a341e58205eb2",
                "short_code": "plat",
                "title": "Alliance Ship",
                "abstract": "Alliance  is a research ship. The 93 meters, 3,180 t NATO ship NRV ALLIANCE was designed in the mid 80’s as a quiet acoustic research platform. It is capable of operating in all oceans strategically important to NATO nations. ALLIANCE enables scientists and engineers from the Centre and partner nations to conduct a wide range of experiments. The ship is equipped with modern scientific instruments, a sophisticated navigation system, and its deck comprises of a vast array of winches (some fitted and some removable), heavy cranes, a lateral frame and a stern U-frame (including a large 4 drum main tow winch for large arrays). This variety of deck equipment allows a large variety of launch and recovery of scientific and engineering sensors, oceanographic instruments, autonomous vehicles and tethered devices."
            },
            "instrument": {
                "ob_id": 31786,
                "uuid": "775e776a78994571b448c29d0647e206",
                "short_code": "instr",
                "title": "WeatherPak",
                "abstract": "The WeatherPak monitoring system supplied by Coastal Environmental Systems is a shipboard weather station designed for harsh environments. Using built in GPS and a compass it is able to calculate true winds (accuracy: +/- 0.3 m/s, resolution: 0.1 m/s) and winds relative to ship motion. It includes meteorological sensors for pressure (+/- 0.2 hPa @ 25°C, 1 hPa), temperature (resolution: 0.2°C), relative humidity (resolution: 1%), pitch, heave and roll. Data is transmitted via ship NMEA system. Data can be recorded up to 1 second time resolution."
            },
            "relatedTo": {
                "ob_id": 31788,
                "uuid": "e0120de39d534374bfa65a6df64126a3",
                "short_code": "acq",
                "title": "Iceland Greenland Seas Project (IGP): surface layer meteorological measurements on board the NATO Research Vessel Alliance",
                "abstract": "Iceland Greenland Seas Project (IGP): surface layer meteorological measurements on board the NATO Research Vessel Alliance"
            }
        },
        {
            "ob_id": 12389,
            "platform": {
                "ob_id": 26503,
                "uuid": "e494bef9ef884794a65a341e58205eb2",
                "short_code": "plat",
                "title": "Alliance Ship",
                "abstract": "Alliance  is a research ship. The 93 meters, 3,180 t NATO ship NRV ALLIANCE was designed in the mid 80’s as a quiet acoustic research platform. It is capable of operating in all oceans strategically important to NATO nations. ALLIANCE enables scientists and engineers from the Centre and partner nations to conduct a wide range of experiments. The ship is equipped with modern scientific instruments, a sophisticated navigation system, and its deck comprises of a vast array of winches (some fitted and some removable), heavy cranes, a lateral frame and a stern U-frame (including a large 4 drum main tow winch for large arrays). This variety of deck equipment allows a large variety of launch and recovery of scientific and engineering sensors, oceanographic instruments, autonomous vehicles and tethered devices."
            },
            "instrument": {
                "ob_id": 31787,
                "uuid": "e0fdc257fd4942b7856db9f061aadc6a",
                "short_code": "instr",
                "title": "SBE38 sea water temperature sensor",
                "abstract": "The Sea-Bird Scientific digital ocean thermometer features an ultra-stable platinum thermistor and state-of-the-art calibration. As on the NATO Research Vessel Alliance, the SBE 38 can be integrated as a remote sensor with an SBE 45 Micro-Thermosalinograph to provide accurate sea surface temperature, conductivity and salinity measurements. Initial accuracy +/- 0.001 °C, resolution 0.00025 °C."
            },
            "relatedTo": {
                "ob_id": 31788,
                "uuid": "e0120de39d534374bfa65a6df64126a3",
                "short_code": "acq",
                "title": "Iceland Greenland Seas Project (IGP): surface layer meteorological measurements on board the NATO Research Vessel Alliance",
                "abstract": "Iceland Greenland Seas Project (IGP): surface layer meteorological measurements on board the NATO Research Vessel Alliance"
            }
        },
        {
            "ob_id": 12390,
            "platform": {
                "ob_id": 31852,
                "uuid": "62d820efce93426dbd499e64b11ac486",
                "short_code": "plat",
                "title": "Drium a'Starraig",
                "abstract": "Drium-A-Starraig station is a Met Office operated site where a C-band weather radar was deployed by the Met Office. It is located near Stornaway, Isle\r\nof Lewis."
            },
            "instrument": {
                "ob_id": 1003,
                "uuid": "fe89d9092055426eb719290ce4063b88",
                "short_code": "instr",
                "title": "Met Office C-band radar",
                "abstract": "UK C Band radar run by the Met Office and the Environment Agency."
            },
            "relatedTo": {
                "ob_id": 31851,
                "uuid": "d445bcf8ebb349bea30631656e6717bc",
                "short_code": "acq",
                "title": "Acquisition Process for: Drium-A-Starraig Rainfall Data from the Met Office Nimrod System",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office C-band radar, NIMROD system; PLATFORMS: Drium-A-Starraig Radar Station, UK;"
            }
        },
        {
            "ob_id": 12391,
            "platform": {
                "ob_id": 31852,
                "uuid": "62d820efce93426dbd499e64b11ac486",
                "short_code": "plat",
                "title": "Drium a'Starraig",
                "abstract": "Drium-A-Starraig station is a Met Office operated site where a C-band weather radar was deployed by the Met Office. It is located near Stornaway, Isle\r\nof Lewis."
            },
            "instrument": {
                "ob_id": 4778,
                "uuid": "5ea91b27324343c38de54cc5aeb98689",
                "short_code": "instr",
                "title": "NIMROD system",
                "abstract": "NIMROD is a very short range forecasting system which integrates nowcasting techniques with Numerical Weather Prediction (NWP) model products to provide forecasts over the UK and surrounding waters up to six hours ahead. NIMROD produces analyses and forecasts of precipitation, cloud and visibility."
            },
            "relatedTo": {
                "ob_id": 31851,
                "uuid": "d445bcf8ebb349bea30631656e6717bc",
                "short_code": "acq",
                "title": "Acquisition Process for: Drium-A-Starraig Rainfall Data from the Met Office Nimrod System",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office C-band radar, NIMROD system; PLATFORMS: Drium-A-Starraig Radar Station, UK;"
            }
        },
        {
            "ob_id": 12392,
            "platform": {
                "ob_id": 31860,
                "uuid": "c07216e49c444f56bfbbdadb26de26eb",
                "short_code": "plat",
                "title": "Agartala Airport",
                "abstract": "Agartala Airport"
            },
            "instrument": {
                "ob_id": 14231,
                "uuid": "490b4a087f734478a243eb9fc5b31a9e",
                "short_code": "instr",
                "title": "Doppler radars",
                "abstract": "A Doppler radar is a specialized radar that uses the Doppler effect to produce velocity data about objects at a distance. It does this by bouncing a microwave signal off a desired target and analyzing how the object's motion has altered the frequency of the returned signal. This variation gives direct and highly accurate measurements of the radial component of a target's velocity relative to the radar. "
            },
            "relatedTo": {
                "ob_id": 31867,
                "uuid": "97840d9e49794b6aad67ac7aebd76272",
                "short_code": "acq",
                "title": "INCOMPASS: IMD Doppler radar convective cell statistics",
                "abstract": "INCOMPASS: IMD Doppler radar convective cell statistics"
            }
        },
        {
            "ob_id": 12393,
            "platform": {
                "ob_id": 31861,
                "uuid": "2c50579b41e24c76b7e995dfd9d69489",
                "short_code": "plat",
                "title": "Bhopal, Raja Bhoj Airport",
                "abstract": "Raja Bhoj Airport"
            },
            "instrument": {
                "ob_id": 14231,
                "uuid": "490b4a087f734478a243eb9fc5b31a9e",
                "short_code": "instr",
                "title": "Doppler radars",
                "abstract": "A Doppler radar is a specialized radar that uses the Doppler effect to produce velocity data about objects at a distance. It does this by bouncing a microwave signal off a desired target and analyzing how the object's motion has altered the frequency of the returned signal. This variation gives direct and highly accurate measurements of the radial component of a target's velocity relative to the radar. "
            },
            "relatedTo": {
                "ob_id": 31867,
                "uuid": "97840d9e49794b6aad67ac7aebd76272",
                "short_code": "acq",
                "title": "INCOMPASS: IMD Doppler radar convective cell statistics",
                "abstract": "INCOMPASS: IMD Doppler radar convective cell statistics"
            }
        },
        {
            "ob_id": 12394,
            "platform": {
                "ob_id": 31862,
                "uuid": "6ebee92684d04907b4566d9d6373c21a",
                "short_code": "plat",
                "title": "Chennai",
                "abstract": "Chennai international airport."
            },
            "instrument": {
                "ob_id": 14231,
                "uuid": "490b4a087f734478a243eb9fc5b31a9e",
                "short_code": "instr",
                "title": "Doppler radars",
                "abstract": "A Doppler radar is a specialized radar that uses the Doppler effect to produce velocity data about objects at a distance. It does this by bouncing a microwave signal off a desired target and analyzing how the object's motion has altered the frequency of the returned signal. This variation gives direct and highly accurate measurements of the radial component of a target's velocity relative to the radar. "
            },
            "relatedTo": {
                "ob_id": 31867,
                "uuid": "97840d9e49794b6aad67ac7aebd76272",
                "short_code": "acq",
                "title": "INCOMPASS: IMD Doppler radar convective cell statistics",
                "abstract": "INCOMPASS: IMD Doppler radar convective cell statistics"
            }
        },
        {
            "ob_id": 12395,
            "platform": {
                "ob_id": 31863,
                "uuid": "5b4c9532af1741b7a36843a39f603099",
                "short_code": "plat",
                "title": "Kolkata",
                "abstract": "Kolkata, Netaji Subhas Chandra Bose International Airport."
            },
            "instrument": {
                "ob_id": 14231,
                "uuid": "490b4a087f734478a243eb9fc5b31a9e",
                "short_code": "instr",
                "title": "Doppler radars",
                "abstract": "A Doppler radar is a specialized radar that uses the Doppler effect to produce velocity data about objects at a distance. It does this by bouncing a microwave signal off a desired target and analyzing how the object's motion has altered the frequency of the returned signal. This variation gives direct and highly accurate measurements of the radial component of a target's velocity relative to the radar. "
            },
            "relatedTo": {
                "ob_id": 31867,
                "uuid": "97840d9e49794b6aad67ac7aebd76272",
                "short_code": "acq",
                "title": "INCOMPASS: IMD Doppler radar convective cell statistics",
                "abstract": "INCOMPASS: IMD Doppler radar convective cell statistics"
            }
        },
        {
            "ob_id": 12396,
            "platform": {
                "ob_id": 31864,
                "uuid": "81180c8f24d84e5bbffa803c539940d9",
                "short_code": "plat",
                "title": "Lucknow",
                "abstract": "Lucknow, Chaudhary Charan Singh International Airport."
            },
            "instrument": {
                "ob_id": 14231,
                "uuid": "490b4a087f734478a243eb9fc5b31a9e",
                "short_code": "instr",
                "title": "Doppler radars",
                "abstract": "A Doppler radar is a specialized radar that uses the Doppler effect to produce velocity data about objects at a distance. It does this by bouncing a microwave signal off a desired target and analyzing how the object's motion has altered the frequency of the returned signal. This variation gives direct and highly accurate measurements of the radial component of a target's velocity relative to the radar. "
            },
            "relatedTo": {
                "ob_id": 31867,
                "uuid": "97840d9e49794b6aad67ac7aebd76272",
                "short_code": "acq",
                "title": "INCOMPASS: IMD Doppler radar convective cell statistics",
                "abstract": "INCOMPASS: IMD Doppler radar convective cell statistics"
            }
        },
        {
            "ob_id": 12397,
            "platform": {
                "ob_id": 31865,
                "uuid": "3beb176aca764de2ad7026fed13f7045",
                "short_code": "plat",
                "title": "Machilipatnam",
                "abstract": "Machilipatnam"
            },
            "instrument": {
                "ob_id": 14231,
                "uuid": "490b4a087f734478a243eb9fc5b31a9e",
                "short_code": "instr",
                "title": "Doppler radars",
                "abstract": "A Doppler radar is a specialized radar that uses the Doppler effect to produce velocity data about objects at a distance. It does this by bouncing a microwave signal off a desired target and analyzing how the object's motion has altered the frequency of the returned signal. This variation gives direct and highly accurate measurements of the radial component of a target's velocity relative to the radar. "
            },
            "relatedTo": {
                "ob_id": 31867,
                "uuid": "97840d9e49794b6aad67ac7aebd76272",
                "short_code": "acq",
                "title": "INCOMPASS: IMD Doppler radar convective cell statistics",
                "abstract": "INCOMPASS: IMD Doppler radar convective cell statistics"
            }
        },
        {
            "ob_id": 12398,
            "platform": {
                "ob_id": 31866,
                "uuid": "779b90c9ac2b4f689fe66be61b3bf381",
                "short_code": "plat",
                "title": "Mumbai",
                "abstract": "Mumbai, Chhatrapati Shivaji International Airport"
            },
            "instrument": {
                "ob_id": 14231,
                "uuid": "490b4a087f734478a243eb9fc5b31a9e",
                "short_code": "instr",
                "title": "Doppler radars",
                "abstract": "A Doppler radar is a specialized radar that uses the Doppler effect to produce velocity data about objects at a distance. It does this by bouncing a microwave signal off a desired target and analyzing how the object's motion has altered the frequency of the returned signal. This variation gives direct and highly accurate measurements of the radial component of a target's velocity relative to the radar. "
            },
            "relatedTo": {
                "ob_id": 31867,
                "uuid": "97840d9e49794b6aad67ac7aebd76272",
                "short_code": "acq",
                "title": "INCOMPASS: IMD Doppler radar convective cell statistics",
                "abstract": "INCOMPASS: IMD Doppler radar convective cell statistics"
            }
        },
        {
            "ob_id": 12399,
            "platform": {
                "ob_id": 30219,
                "uuid": "07a71f4e62e2468391f492b85905167c",
                "short_code": "plat",
                "title": "Indira Gandhi Delhi Technical University for Women (IGDTUW)",
                "abstract": "Indira Gandhi Delhi Technical University for Women (IGDTUW) which is situated on the periphery of Old Delhi and overlooks a very heavily populated area. As part of the DelhiFlux project the team have constructed a rooftop mast at 4m and a 30 m tall flux tower from which to directly measure pollutant emissions from two contrasting regions of Delhi."
            },
            "instrument": {
                "ob_id": 27168,
                "uuid": "d90c2ff4219441f78ecdea981a33ed36",
                "short_code": "instr",
                "title": "University of York High Volume Sampler (Ecotech 3000, Australia)",
                "abstract": "The HiVol 3000 particulate sampler performs remote unattended sampling of PM2.5, PM10 or TSP along with basic meteorological parameters."
            },
            "relatedTo": {
                "ob_id": 31871,
                "uuid": "11a725a0f1ef40acb5cbe4b619505ba8",
                "short_code": "acq",
                "title": "APHH: Ionic species data within PM2.5 measurements made at the Indira Gandhi Delhi Technical University for Women (IGDTUW) site during the pre and post monsoon periods for the DelhiFlux field campaign 2018",
                "abstract": "APHH: Ionic species data within PM2.5 measurements made at the Indira Gandhi Delhi Technical University for Women (IGDTUW) site during the pre and post monsoon periods for the DelhiFlux field campaign 2018"
            }
        },
        {
            "ob_id": 12400,
            "platform": {
                "ob_id": 30219,
                "uuid": "07a71f4e62e2468391f492b85905167c",
                "short_code": "plat",
                "title": "Indira Gandhi Delhi Technical University for Women (IGDTUW)",
                "abstract": "Indira Gandhi Delhi Technical University for Women (IGDTUW) which is situated on the periphery of Old Delhi and overlooks a very heavily populated area. As part of the DelhiFlux project the team have constructed a rooftop mast at 4m and a 30 m tall flux tower from which to directly measure pollutant emissions from two contrasting regions of Delhi."
            },
            "instrument": {
                "ob_id": 27169,
                "uuid": "f104d5769a8543dca6c2c90dde6e18a6",
                "short_code": "instr",
                "title": "University of York Dionex ICS-1100 Ion Chromatography System",
                "abstract": "The Thermo Scientific Dionex ICS-1100 Ion Chromatography System (Dionex ICS-1100) performs ion analyses using suppressed or non-suppressed conductivity detection. An ion chromatography system typically consists of a liquid eluent, a high-pressure pump, a sample injector, a guard and separator column, a chemical suppressor, a conductivity cell, and a data collection system."
            },
            "relatedTo": {
                "ob_id": 31871,
                "uuid": "11a725a0f1ef40acb5cbe4b619505ba8",
                "short_code": "acq",
                "title": "APHH: Ionic species data within PM2.5 measurements made at the Indira Gandhi Delhi Technical University for Women (IGDTUW) site during the pre and post monsoon periods for the DelhiFlux field campaign 2018",
                "abstract": "APHH: Ionic species data within PM2.5 measurements made at the Indira Gandhi Delhi Technical University for Women (IGDTUW) site during the pre and post monsoon periods for the DelhiFlux field campaign 2018"
            }
        },
        {
            "ob_id": 12401,
            "platform": {
                "ob_id": 31876,
                "uuid": "184c930b206744e8b80321dd9024af64",
                "short_code": "plat",
                "title": "TANSAT",
                "abstract": "The TANSAT Satellite (Full name: Exploratory Satellite for Atmospheric CO2) is a Chinese satellite dedicated to the measurment of Atmospheric CO2.   It was launched in December 2016."
            },
            "instrument": {
                "ob_id": 31877,
                "uuid": "57fe77686e4f4e64b42b48617e726410",
                "short_code": "instr",
                "title": "ACGS",
                "abstract": "The Atmospheric Carbon-dioxide Grating Spectrometer (ACGS) is one of the instruments on the Chinese TANSAT satellite.   It is a three-band NIR / SWIR grating spectroradiometer designed for the measurement of total-column CO2."
            },
            "relatedTo": {
                "ob_id": 31875,
                "uuid": "ca5b979b19204cb19c7865ace44b6328",
                "short_code": "acq",
                "title": "Aquisition for ESA Greenhouse Gases Climate Change Initiative (GHG_cci): Column-averaged carbon dioxide from TANSAT, generated with the OCFP algorithm, version 1.0",
                "abstract": "Aquisition for ESA Greenhouse Gases Climate Change Initiative (GHG_cci): Column-averaged carbon dioxide from TANSAT, generated with the OCFP algorithm, version 1.0"
            }
        },
        {
            "ob_id": 12402,
            "platform": {
                "ob_id": 31882,
                "uuid": "c666fb3d29f040f98ce4ae30db74bf50",
                "short_code": "plat",
                "title": "Northwest Iceland Sea - Eggvin Offset",
                "abstract": "Location of SEAWATCH Wavescan Buoy adjacent to subsurface mooring in hte Eggvin Offset. Used in the Iceland Greenland seas Project (IGP)"
            },
            "instrument": {
                "ob_id": 31881,
                "uuid": "f115f2e2014a47a7a6449b2ad581570d",
                "short_code": "instr",
                "title": "SEAWATCH Wavescan buoy",
                "abstract": "Measures standard meteorological variables, sea surface temperature, surface ocean  currents and wave height, direction and period."
            },
            "relatedTo": {
                "ob_id": 31880,
                "uuid": "2a4d32750386446894e7da60d92d401d",
                "short_code": "acq",
                "title": "Iceland Greenland seas Project (IGP): Meteorological Buoy Measurements",
                "abstract": "Iceland Greenland seas Project (IGP): Meteorological Buoy Measurements"
            }
        },
        {
            "ob_id": 12403,
            "platform": {
                "ob_id": 817,
                "uuid": "0d60dd064b6449b09f5c7fd4c41bd693",
                "short_code": "plat",
                "title": "NCAS Chilbolton Atmospheric Observatory (CAO)",
                "abstract": "The National Centre for Atmospheric Science's Chilbolton Atmospheric Observatory, formerly known as the Chilbolton Facility for Atmospheric and Radio Research (CFARR), is hosted by the Science and Technology Facilities Council (STFC) in rural Hampshire in the South of England.  Through a combination of long-term observations and tailored operations it provides national capability for the study of clouds, rainfall, boundary-layer processes and aerosols, and is particularly well suited as a site for hosting field campaigns involving visiting instruments.\r\n\r\nThe CAO site is located one mile south of Chilbolton Village, 6 miles south of Andover, Hampshire. The site was used as an airfield during the Second World War and is relatively flat and slightly elevated above the surrounding area.\r\n\r\nThe observatory operates more than twenty major instruments, many continuously, while others are available on-demand according to user configuration requirements. The portfolio includes a powerful combination of dual-polarisation Doppler radars, lidars, radiometers, and supporting instruments; the continuous round-the-clock operation of lidar and cloud radar instruments at Chilbolton is unique within the UK. These are supplemented by a suite of meteorological instrumentation including rain gauges, and disdrometers.  A multi-wavelength sun photometer provides continuous measurements of aerosol optical depth in clear skies, and contributes to the Aerosol Robotic Network (AERONET).\r\n\r\nThe Chilbolton Advanced Meteorological Radar (CAMRa) is mounted on a 25-metre, fully steerable antenna, and is able to probe clouds and storms with unparalleled sensitivity and resolution. In addition, zenith-pointing polarimetric, Doppler 35 GHz and 94 GHz cloud radars are routinely operated for detailed microphysical studies of cloud processes and cloud climatology.  A transportable, scanning 35 GHz cloud radar system is also hosted at Chilbolton, further enhancing the available capability.\r\n\r\nChilbolton was one of the pilot cloud profiling sites for the CLOUDNET project, and continues to make observations that feed into the Aerosol Clouds and Trace Gases Research Infrastructure (ACTRIS).   Capability at the site will be enhanced in the next few years, with the incorporation of a Raman lidar, with the ambition being for this to form an ACTRIS observational platform for aerosol profiling.\r\n\r\nThe presence (since January 2016) of a Defra air quality monitoring supersite at the observatory site (providing rural background measurements as part of national and transboundary networks) offers the research community further excellent opportunities for intercomparison campaigns and instrument evaluation.\r\n\r\nWIGOS id: \r\n0-826-300-3\r\n0-826-300-4\r\n0-826-300-5\r\n\r\nThe Met Office also operated a boundary layer wind profiler at the site (now operated by NCAS AMOF), for which the site was given a WMO ID 03754."
            },
            "instrument": {
                "ob_id": 12250,
                "uuid": "792da2ff61f647aa8021b4b9c06702a9",
                "short_code": "instr",
                "title": "NCAS Atmospheric Measurement Facility's (AMOF) mobile X-band radar 1",
                "abstract": "The National Centre for Atmospheric Science Atmospheric Measurement Facility's (NCAS AMOF) mobile X-band radar operates in the X-band (frequency = 9.375 GHz, wavelength = 3 cm). It has Doppler and dual-polarisation capability. The radar measures the location and intensity of precipitation, radial winds and polarisation parameters. It works by transmitting pulses of electromagnetic radiation and measuring the amount of energy backscattered to the receiver. The time delay between the transmitted and received pulses enables the range of the object to be determined. In the case of precipitation, the magnitude of the backscattered signal is proportional to the size and number of raindrops. The radar also measures the radial velocity through the Doppler effect. In the absence of precipitation, the radar is sensitive to backscattering from insects, known as clear-air echoes, at close range. These signals provide information on the wind field and the organisation of the boundary-layer e.g. features such as convergence lines can be identified. In addition, the radar has dual-polarisation capability; it simultaneously transmits and receives horizontally- and vertically- polarised waves. Through this technique the radar measures a number of additional variables that provide information on the size and shape of precipitation, identification of non-meteorological echoes, attenuation (a decrease in the signal strength due to the absorption and scattering of the radar signal as it propagates through heavy rain), and alternative methods for calculating rainfall rates. \r\n\r\nThe system has a conventional parabolic antenna of 2.4m diameter and a beamwidth of 1 degree (in the horizontal and vertical), and is operated without a radome. The range resolution is tunable and dependent on the user-selected pulse width (0.5, 1 or 2 micro seconds) and pulse repetition frequency (PRF, 250-2000 Hz). The radar is fully transportable, being mounted on a trailer approved for EU roads that can be towed by a 4x4 vehicle. Signal analysis, data retrievals and data storage are performed by PCs contained within the trailer unit. The radar can be operated via a laptop that connects by wireless, ethernet or 3G to the onboard PCs. The operational software allows the user to set up the radar for deployment and schedule the scanning sequence. The software also provides real-time data visualisation and product generation.\r\n\r\nThe data frequency is dependant on the requirements for the instrument's deployment, but is typically of the order of 10 360-degree scans at various elevations every 5 minutes.\r\n\r\nParameters available in data files from this instrument include: \r\nDOP  - degree of polarization; \r\nKDP  - specific differential phase shift; \r\nPhiDP -  differential phase shift; \r\nRhoHV - co-polar cross correlation coefficient; \r\nSQI - signal quality index or normalized_coherent_power; \r\nV - radial velocity; \r\nW - spectral width; \r\nZDR - differential reflectivity; \r\ndBZ - reflectivity or equivalent reflectivity factor."
            },
            "relatedTo": {
                "ob_id": 31950,
                "uuid": "2bab7d6879dc408db2d2a54d2bb2673b",
                "short_code": "acq",
                "title": "NCAS-Xband radar longterm  measurements from 08/11/2016-24/05/2018 at Chilbolton",
                "abstract": "NCAS-Xband radar longterm  measurements from 08/11/2016-24/05/2018 at Chilbolton Observatory"
            }
        },
        {
            "ob_id": 12404,
            "platform": {
                "ob_id": 30018,
                "uuid": "dc9445f2ebc5410cb39df2984165c52b",
                "short_code": "plat",
                "title": "JASON-1",
                "abstract": "The JASON-1 (Joint Altimetery Satellite Oceanography Network - 1) satellite was the first flight of the JASON series of satellites, with a primary mission to study ocean topography and waves.   It flew between December 2001 and July 2013"
            },
            "instrument": {
                "ob_id": 30019,
                "uuid": "64d73638c9a14a3fad59d6ae8658fd37",
                "short_code": "instr",
                "title": "Poseidon-2",
                "abstract": "The Poseidon-2 satellite instrument was flown on the JASON-1 satellite.  It is a radar altimeter designed to study ocean topography, significant wave height and wind speed."
            },
            "relatedTo": {
                "ob_id": 31953,
                "uuid": "1a4fe170b116409bb7177cb098b7cb8f",
                "short_code": "acq",
                "title": "Acquisition for the ESA Climate Change Initiative Sea Level altimeter coastal sea level anomalies datasets",
                "abstract": "Acquisition for the ESA Climate Change Initiative Sea Level altimeter coastal sea level anomalies datasets"
            }
        },
        {
            "ob_id": 12405,
            "platform": {
                "ob_id": 30020,
                "uuid": "154dafa0c39d47beb7b1b8f29efa237f",
                "short_code": "plat",
                "title": "JASON-2",
                "abstract": "The JASON-2 (Joint Altimetry Satellite Oceanography Network -2 ) satellite was flown to study ocean topography and waves.  It flew between June 2008 and October 2019"
            },
            "instrument": {
                "ob_id": 30021,
                "uuid": "57297602ceef42edb983796ce9089963",
                "short_code": "instr",
                "title": "Poseidon-3",
                "abstract": "The Poseidon-3 instrument was flown on the JASON-2 satellite.  It is a radar altimeter, designed to study ocean topography, significant wave height and wind speed."
            },
            "relatedTo": {
                "ob_id": 31953,
                "uuid": "1a4fe170b116409bb7177cb098b7cb8f",
                "short_code": "acq",
                "title": "Acquisition for the ESA Climate Change Initiative Sea Level altimeter coastal sea level anomalies datasets",
                "abstract": "Acquisition for the ESA Climate Change Initiative Sea Level altimeter coastal sea level anomalies datasets"
            }
        },
        {
            "ob_id": 12406,
            "platform": {
                "ob_id": 30022,
                "uuid": "40826d62fbe6438494c543d9284e7c61",
                "short_code": "plat",
                "title": "JASON-3",
                "abstract": "The JASON-3 (Joint Altimetry Satellite Oceanography Network - 3 ) Satellite was launched on Jan 2016.  It primary mission is to study ocean topography and waves."
            },
            "instrument": {
                "ob_id": 30023,
                "uuid": "fcdd312219c4443985a9a1708867500e",
                "short_code": "instr",
                "title": "Poseidon-3B",
                "abstract": "The Poseidon-3B satellite instrument is flying on the JASON-3 satellite.   It is a radar altimeter, designed to study ocean topography, significant wave height and wind speed."
            },
            "relatedTo": {
                "ob_id": 31953,
                "uuid": "1a4fe170b116409bb7177cb098b7cb8f",
                "short_code": "acq",
                "title": "Acquisition for the ESA Climate Change Initiative Sea Level altimeter coastal sea level anomalies datasets",
                "abstract": "Acquisition for the ESA Climate Change Initiative Sea Level altimeter coastal sea level anomalies datasets"
            }
        },
        {
            "ob_id": 12407,
            "platform": {
                "ob_id": 8207,
                "uuid": "3f2dbe69fe4c40ee9e1e8be87e15a1d5",
                "short_code": "plat",
                "title": "Metop-A",
                "abstract": "Metop-A, launched on 19 October 2006, represents the first in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS). Metop-A is Europe's first polar-orbiting meteorological satellite"
            },
            "instrument": {
                "ob_id": 27121,
                "uuid": "ca133e0771514003a9e7c2462c1b363c",
                "short_code": "instr",
                "title": "ASCAT",
                "abstract": "ASCAT (Advanced Scatterometer)  is a C Band (2.55 GHz) Scatterometer flown on the Metop series of satellites.  It measures the sea surface wind vecotr and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 32011,
                "uuid": "3b5a15073de0478ba33964ebb063ecb6",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Active product, v05.2",
                "abstract": "The ESA Climate Change Initiative Active product has been derived from data from the AMI-WS and ASCAT satellite instruments."
            }
        },
        {
            "ob_id": 12408,
            "platform": {
                "ob_id": 8299,
                "uuid": "84a6355ac58249cc8c636e77a243c86a",
                "short_code": "plat",
                "title": "Metop-B",
                "abstract": "Metop-B, launched on the 17th September 2012, is the second in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS)."
            },
            "instrument": {
                "ob_id": 27121,
                "uuid": "ca133e0771514003a9e7c2462c1b363c",
                "short_code": "instr",
                "title": "ASCAT",
                "abstract": "ASCAT (Advanced Scatterometer)  is a C Band (2.55 GHz) Scatterometer flown on the Metop series of satellites.  It measures the sea surface wind vecotr and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 32011,
                "uuid": "3b5a15073de0478ba33964ebb063ecb6",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Active product, v05.2",
                "abstract": "The ESA Climate Change Initiative Active product has been derived from data from the AMI-WS and ASCAT satellite instruments."
            }
        },
        {
            "ob_id": 12409,
            "platform": {
                "ob_id": 7805,
                "uuid": "d21630e98aa74a4f8406743b74e5d076",
                "short_code": "plat",
                "title": "ERS-1",
                "abstract": "The European Remote Sensing satellite 1 (ERS1) was launched on 17th July 1991 and was the first flight of the RSA ERS program.  The payload included the ATSR, AMU-SAR , AMI-SCAT, LRR PRARE and RA instruments.  End of mission for ERS1 was 10th March 2000."
            },
            "instrument": {
                "ob_id": 27122,
                "uuid": "7b488736a173477689480990d5b38aa9",
                "short_code": "instr",
                "title": "AMI-SCAT",
                "abstract": "AMI-SCAT (Active Microwave Instrument - Scatterometer) is a C-band (5.3 GHz) scatterometer flying on the ERS-1 and ERS-2 satellites.  It measures the sea surface wind vector and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 32011,
                "uuid": "3b5a15073de0478ba33964ebb063ecb6",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Active product, v05.2",
                "abstract": "The ESA Climate Change Initiative Active product has been derived from data from the AMI-WS and ASCAT satellite instruments."
            }
        },
        {
            "ob_id": 12410,
            "platform": {
                "ob_id": 7813,
                "uuid": "8ee876e1ea644ed7a81d4e3536133fa0",
                "short_code": "plat",
                "title": "European Remote Sensing satellite 2 - ERS-2",
                "abstract": "ESA's two European Remote Sensing (ERS) satellites, ERS-1 and –2, were launched into the same orbit in 1991 and 1995 respectively. Their payloads included a synthetic aperture imaging radar, radar altimeter and instruments to measure ocean surface temperature and wind fields.\r\n\r\nERS-2 added an additional sensor for atmospheric ozone monitoring. The two satellites acquired a combined data set extending over two decades.\r\n\r\nThe ERS-2 satellite was retired on 05 September 2011."
            },
            "instrument": {
                "ob_id": 27122,
                "uuid": "7b488736a173477689480990d5b38aa9",
                "short_code": "instr",
                "title": "AMI-SCAT",
                "abstract": "AMI-SCAT (Active Microwave Instrument - Scatterometer) is a C-band (5.3 GHz) scatterometer flying on the ERS-1 and ERS-2 satellites.  It measures the sea surface wind vector and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 32011,
                "uuid": "3b5a15073de0478ba33964ebb063ecb6",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Active product, v05.2",
                "abstract": "The ESA Climate Change Initiative Active product has been derived from data from the AMI-WS and ASCAT satellite instruments."
            }
        },
        {
            "ob_id": 12411,
            "platform": {
                "ob_id": 458,
                "uuid": "b6d87ac1455348cd97a4386b38995dbb",
                "short_code": "plat",
                "title": "NIMBUS 7 Satellite",
                "abstract": "The NASA Nimbus 7 research-and-development polar-orbiting satellite served as a stabilized, earth-oriented platform for the testing of advanced systems for sensing and collecting data in the pollution, oceanographic and meteorological disciplines. It was launched on October 24, 1978."
            },
            "instrument": {
                "ob_id": 2636,
                "uuid": "1578228cc3cf4b9fba0b88c61b58800b",
                "short_code": "instr",
                "title": "Scanning Multichannel Microwave Radiometer (SMMR)",
                "abstract": "The Scanning Multichannel Microwave Radiometer operated on NASA's Nimbus-7 satellite for more than eight years, from 26 October 1978 to 20 August 1987, transmitting data every other day. Intended to obtain ocean circulation parameters such as sea surface temperatures, low altitude winds, water vapor and cloud liquid water content on an all-weather basis, the SMMR is a ten channel instrument capable of receiving both horizontally and vertically polarized radiation. A parabolic antenna 79 cm in diameter reflected microwave emissions into a five-frequency feed horn. The antenna beam maintained a constant nadir angle of 42 degrees, resulting in an incidence angle of 50.3 degrees at Earth's surface. The antenna was forward viewing and rotated equally +/- 25 degrees about the satellite subtrack. The 50 degree scan provided a 780 km swath of the Earth's surface. Scan period was 4.096 seconds."
            },
            "relatedTo": {
                "ob_id": 32012,
                "uuid": "8e5d8bc49927483286faa5929e012d72",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Passive product, v05.2",
                "abstract": "The ESA Climate Change Initiative Passive product has been derived from data from the SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 , MIRAS (SMOS) and SMAP satellite instruments."
            }
        },
        {
            "ob_id": 12412,
            "platform": {
                "ob_id": 2629,
                "uuid": "9f1b0a2380cc47919b201880e0fee6de",
                "short_code": "plat",
                "title": "Defense Meteorological Satellite Program (DMSP) Satellites",
                "abstract": "DMSP satellites are used for strategic and tactical weather prediction to aid the U.S. military in planning operations at sea, on land and in the air. Equipped with a sophisticated sensor suite that can image visible and infrared cloud cover and measure precipitation, surface temperature, and soil moisture, the satellite collects specialized global meteorological, oceanographic, and solar-geophysical information in all weather conditions. The DMSP constellation comprises two spacecraft in near-polar orbits, C3 (command, control and communications), user terminals and weather centers."
            },
            "instrument": {
                "ob_id": 2630,
                "uuid": "54f897597ec04c09b01095eb05c7419e",
                "short_code": "instr",
                "title": "Special Sensor Microwave / Imager (SSM/I)",
                "abstract": "The SSM/I is a seven-channel, four frequency, linearly-polarized, passive microwave radiometric system which measures atmospheric, ocean and terrain microwave brightness temperatures at 19.35, 22.235, 37.0 and 85.5 GHz. The data are used to obtain synoptic maps of critical atmospheric, oceanographic and selected land parameters on a global scale."
            },
            "relatedTo": {
                "ob_id": 32012,
                "uuid": "8e5d8bc49927483286faa5929e012d72",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Passive product, v05.2",
                "abstract": "The ESA Climate Change Initiative Passive product has been derived from data from the SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 , MIRAS (SMOS) and SMAP satellite instruments."
            }
        },
        {
            "ob_id": 12413,
            "platform": {
                "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."
            },
            "instrument": {
                "ob_id": 27126,
                "uuid": "9173171ba44845e9a873e21b4dee19e2",
                "short_code": "instr",
                "title": "TMI",
                "abstract": "TMI (TRMM  Microwave Imager) is a multi-purpose microwave imager flying on the TRMM (Tropical Rainfall Measuring Mission)."
            },
            "relatedTo": {
                "ob_id": 32012,
                "uuid": "8e5d8bc49927483286faa5929e012d72",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Passive product, v05.2",
                "abstract": "The ESA Climate Change Initiative Passive product has been derived from data from the SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 , MIRAS (SMOS) and SMAP satellite instruments."
            }
        },
        {
            "ob_id": 12414,
            "platform": {
                "ob_id": 10906,
                "uuid": "5a1076bffc8c4c5d8a2ff3a4cfb29846",
                "short_code": "plat",
                "title": "Aqua Satellite, part of the Earth Observation System Afternoon Constellation (EOS-PM)",
                "abstract": "Aqua, launched on 4th April 2002, is a polar-orbiting satellite within the Afternoon Constellation (A-Train) that have equator crossings around 13:30 and 01:30 under NASA's Earth Obseration System (EOS). The satellite carries Atmospheric Infrared Sounder (AIRS), Advanced Microwave Sounding Unit (AMSU-A), Humidity Sounder for Brazil (HSB), Advanced Microwave Scanning Radiometer for EOS (AMSR-E), Moderate-Resolution Imaging Spectroradiometer (MODIS) and Clouds and the Earth's Radiant Energy System (CERES), and these collect data on the Earth's atmospheric conditions, snow and ice, sea surface temperature and ocean productivity, and soil moisture.   Aqua was the first member launched of a group of satellites termed the Afternoon Constellation, or sometimes the A-Train. "
            },
            "instrument": {
                "ob_id": 14485,
                "uuid": "77dd26fc341a440b85a98fe95b1976f8",
                "short_code": "instr",
                "title": "AMSR-E",
                "abstract": "Advanced Microwave Scanning Radiometer for EOS"
            },
            "relatedTo": {
                "ob_id": 32012,
                "uuid": "8e5d8bc49927483286faa5929e012d72",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Passive product, v05.2",
                "abstract": "The ESA Climate Change Initiative Passive product has been derived from data from the SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 , MIRAS (SMOS) and SMAP satellite instruments."
            }
        },
        {
            "ob_id": 12415,
            "platform": {
                "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."
            },
            "instrument": {
                "ob_id": 25272,
                "uuid": "a6002da7c0954ce0aa146c1b24877a0a",
                "short_code": "instr",
                "title": "AMSR-2",
                "abstract": "Advanced Microwave Scanning Radiometer -2, flying on the Global Change Observation Mission (GCOM) series of satellites flown by JAXA"
            },
            "relatedTo": {
                "ob_id": 32012,
                "uuid": "8e5d8bc49927483286faa5929e012d72",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Passive product, v05.2",
                "abstract": "The ESA Climate Change Initiative Passive product has been derived from data from the SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 , MIRAS (SMOS) and SMAP satellite instruments."
            }
        },
        {
            "ob_id": 12416,
            "platform": {
                "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)"
            },
            "instrument": {
                "ob_id": 27125,
                "uuid": "10f4aca379f84e0cae56392a85604469",
                "short_code": "instr",
                "title": "WindSat",
                "abstract": "WindSat is a passive microwave radiometer flown on the Coriolis Satellite by the US Department of Defence since 2003."
            },
            "relatedTo": {
                "ob_id": 32012,
                "uuid": "8e5d8bc49927483286faa5929e012d72",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Passive product, v05.2",
                "abstract": "The ESA Climate Change Initiative Passive product has been derived from data from the SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 , MIRAS (SMOS) and SMAP satellite instruments."
            }
        },
        {
            "ob_id": 12417,
            "platform": {
                "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."
            },
            "instrument": {
                "ob_id": 27124,
                "uuid": "9b4be0d67030450ca8aebf37cf39500c",
                "short_code": "instr",
                "title": "MIRAS",
                "abstract": "MIRAS (Microwave Imaging Radiometer using Aperture Synthesis) is an European Space Agency instrument flown on the SMOS (Soil Moisture and Ocean Salinity) Satellite.  It measures Ocean Salinity and Soil Moisture."
            },
            "relatedTo": {
                "ob_id": 32012,
                "uuid": "8e5d8bc49927483286faa5929e012d72",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Passive product, v05.2",
                "abstract": "The ESA Climate Change Initiative Passive product has been derived from data from the SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 , MIRAS (SMOS) and SMAP satellite instruments."
            }
        },
        {
            "ob_id": 12418,
            "platform": {
                "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."
            },
            "instrument": {
                "ob_id": 27124,
                "uuid": "9b4be0d67030450ca8aebf37cf39500c",
                "short_code": "instr",
                "title": "MIRAS",
                "abstract": "MIRAS (Microwave Imaging Radiometer using Aperture Synthesis) is an European Space Agency instrument flown on the SMOS (Soil Moisture and Ocean Salinity) Satellite.  It measures Ocean Salinity and Soil Moisture."
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12419,
            "platform": {
                "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)"
            },
            "instrument": {
                "ob_id": 27125,
                "uuid": "10f4aca379f84e0cae56392a85604469",
                "short_code": "instr",
                "title": "WindSat",
                "abstract": "WindSat is a passive microwave radiometer flown on the Coriolis Satellite by the US Department of Defence since 2003."
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12420,
            "platform": {
                "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."
            },
            "instrument": {
                "ob_id": 25272,
                "uuid": "a6002da7c0954ce0aa146c1b24877a0a",
                "short_code": "instr",
                "title": "AMSR-2",
                "abstract": "Advanced Microwave Scanning Radiometer -2, flying on the Global Change Observation Mission (GCOM) series of satellites flown by JAXA"
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12421,
            "platform": {
                "ob_id": 10906,
                "uuid": "5a1076bffc8c4c5d8a2ff3a4cfb29846",
                "short_code": "plat",
                "title": "Aqua Satellite, part of the Earth Observation System Afternoon Constellation (EOS-PM)",
                "abstract": "Aqua, launched on 4th April 2002, is a polar-orbiting satellite within the Afternoon Constellation (A-Train) that have equator crossings around 13:30 and 01:30 under NASA's Earth Obseration System (EOS). The satellite carries Atmospheric Infrared Sounder (AIRS), Advanced Microwave Sounding Unit (AMSU-A), Humidity Sounder for Brazil (HSB), Advanced Microwave Scanning Radiometer for EOS (AMSR-E), Moderate-Resolution Imaging Spectroradiometer (MODIS) and Clouds and the Earth's Radiant Energy System (CERES), and these collect data on the Earth's atmospheric conditions, snow and ice, sea surface temperature and ocean productivity, and soil moisture.   Aqua was the first member launched of a group of satellites termed the Afternoon Constellation, or sometimes the A-Train. "
            },
            "instrument": {
                "ob_id": 14485,
                "uuid": "77dd26fc341a440b85a98fe95b1976f8",
                "short_code": "instr",
                "title": "AMSR-E",
                "abstract": "Advanced Microwave Scanning Radiometer for EOS"
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12422,
            "platform": {
                "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."
            },
            "instrument": {
                "ob_id": 27126,
                "uuid": "9173171ba44845e9a873e21b4dee19e2",
                "short_code": "instr",
                "title": "TMI",
                "abstract": "TMI (TRMM  Microwave Imager) is a multi-purpose microwave imager flying on the TRMM (Tropical Rainfall Measuring Mission)."
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12423,
            "platform": {
                "ob_id": 2629,
                "uuid": "9f1b0a2380cc47919b201880e0fee6de",
                "short_code": "plat",
                "title": "Defense Meteorological Satellite Program (DMSP) Satellites",
                "abstract": "DMSP satellites are used for strategic and tactical weather prediction to aid the U.S. military in planning operations at sea, on land and in the air. Equipped with a sophisticated sensor suite that can image visible and infrared cloud cover and measure precipitation, surface temperature, and soil moisture, the satellite collects specialized global meteorological, oceanographic, and solar-geophysical information in all weather conditions. The DMSP constellation comprises two spacecraft in near-polar orbits, C3 (command, control and communications), user terminals and weather centers."
            },
            "instrument": {
                "ob_id": 2630,
                "uuid": "54f897597ec04c09b01095eb05c7419e",
                "short_code": "instr",
                "title": "Special Sensor Microwave / Imager (SSM/I)",
                "abstract": "The SSM/I is a seven-channel, four frequency, linearly-polarized, passive microwave radiometric system which measures atmospheric, ocean and terrain microwave brightness temperatures at 19.35, 22.235, 37.0 and 85.5 GHz. The data are used to obtain synoptic maps of critical atmospheric, oceanographic and selected land parameters on a global scale."
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12424,
            "platform": {
                "ob_id": 458,
                "uuid": "b6d87ac1455348cd97a4386b38995dbb",
                "short_code": "plat",
                "title": "NIMBUS 7 Satellite",
                "abstract": "The NASA Nimbus 7 research-and-development polar-orbiting satellite served as a stabilized, earth-oriented platform for the testing of advanced systems for sensing and collecting data in the pollution, oceanographic and meteorological disciplines. It was launched on October 24, 1978."
            },
            "instrument": {
                "ob_id": 2636,
                "uuid": "1578228cc3cf4b9fba0b88c61b58800b",
                "short_code": "instr",
                "title": "Scanning Multichannel Microwave Radiometer (SMMR)",
                "abstract": "The Scanning Multichannel Microwave Radiometer operated on NASA's Nimbus-7 satellite for more than eight years, from 26 October 1978 to 20 August 1987, transmitting data every other day. Intended to obtain ocean circulation parameters such as sea surface temperatures, low altitude winds, water vapor and cloud liquid water content on an all-weather basis, the SMMR is a ten channel instrument capable of receiving both horizontally and vertically polarized radiation. A parabolic antenna 79 cm in diameter reflected microwave emissions into a five-frequency feed horn. The antenna beam maintained a constant nadir angle of 42 degrees, resulting in an incidence angle of 50.3 degrees at Earth's surface. The antenna was forward viewing and rotated equally +/- 25 degrees about the satellite subtrack. The 50 degree scan provided a 780 km swath of the Earth's surface. Scan period was 4.096 seconds."
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12425,
            "platform": {
                "ob_id": 8207,
                "uuid": "3f2dbe69fe4c40ee9e1e8be87e15a1d5",
                "short_code": "plat",
                "title": "Metop-A",
                "abstract": "Metop-A, launched on 19 October 2006, represents the first in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS). Metop-A is Europe's first polar-orbiting meteorological satellite"
            },
            "instrument": {
                "ob_id": 27121,
                "uuid": "ca133e0771514003a9e7c2462c1b363c",
                "short_code": "instr",
                "title": "ASCAT",
                "abstract": "ASCAT (Advanced Scatterometer)  is a C Band (2.55 GHz) Scatterometer flown on the Metop series of satellites.  It measures the sea surface wind vecotr and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12426,
            "platform": {
                "ob_id": 8299,
                "uuid": "84a6355ac58249cc8c636e77a243c86a",
                "short_code": "plat",
                "title": "Metop-B",
                "abstract": "Metop-B, launched on the 17th September 2012, is the second in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS)."
            },
            "instrument": {
                "ob_id": 27121,
                "uuid": "ca133e0771514003a9e7c2462c1b363c",
                "short_code": "instr",
                "title": "ASCAT",
                "abstract": "ASCAT (Advanced Scatterometer)  is a C Band (2.55 GHz) Scatterometer flown on the Metop series of satellites.  It measures the sea surface wind vecotr and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12427,
            "platform": {
                "ob_id": 7805,
                "uuid": "d21630e98aa74a4f8406743b74e5d076",
                "short_code": "plat",
                "title": "ERS-1",
                "abstract": "The European Remote Sensing satellite 1 (ERS1) was launched on 17th July 1991 and was the first flight of the RSA ERS program.  The payload included the ATSR, AMU-SAR , AMI-SCAT, LRR PRARE and RA instruments.  End of mission for ERS1 was 10th March 2000."
            },
            "instrument": {
                "ob_id": 27122,
                "uuid": "7b488736a173477689480990d5b38aa9",
                "short_code": "instr",
                "title": "AMI-SCAT",
                "abstract": "AMI-SCAT (Active Microwave Instrument - Scatterometer) is a C-band (5.3 GHz) scatterometer flying on the ERS-1 and ERS-2 satellites.  It measures the sea surface wind vector and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12428,
            "platform": {
                "ob_id": 7813,
                "uuid": "8ee876e1ea644ed7a81d4e3536133fa0",
                "short_code": "plat",
                "title": "European Remote Sensing satellite 2 - ERS-2",
                "abstract": "ESA's two European Remote Sensing (ERS) satellites, ERS-1 and –2, were launched into the same orbit in 1991 and 1995 respectively. Their payloads included a synthetic aperture imaging radar, radar altimeter and instruments to measure ocean surface temperature and wind fields.\r\n\r\nERS-2 added an additional sensor for atmospheric ozone monitoring. The two satellites acquired a combined data set extending over two decades.\r\n\r\nThe ERS-2 satellite was retired on 05 September 2011."
            },
            "instrument": {
                "ob_id": 27122,
                "uuid": "7b488736a173477689480990d5b38aa9",
                "short_code": "instr",
                "title": "AMI-SCAT",
                "abstract": "AMI-SCAT (Active Microwave Instrument - Scatterometer) is a C-band (5.3 GHz) scatterometer flying on the ERS-1 and ERS-2 satellites.  It measures the sea surface wind vector and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12429,
            "platform": {
                "ob_id": 29941,
                "uuid": "2b126b39dbb64c0681f12b68f2308fee",
                "short_code": "plat",
                "title": "SMAP",
                "abstract": "The Soil Moisture Active-Passive (SMAP) satelliteis a NASA satellite launched in 2015."
            },
            "instrument": {
                "ob_id": 29938,
                "uuid": "e050ad22e3b943f9a5f1563a1e6fb82c",
                "short_code": "instr",
                "title": "SMAP",
                "abstract": "The Soil Moisture Active Passive instrument is a microwave radiometer flown on the NASA SMAP satellite."
            },
            "relatedTo": {
                "ob_id": 32012,
                "uuid": "8e5d8bc49927483286faa5929e012d72",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Passive product, v05.2",
                "abstract": "The ESA Climate Change Initiative Passive product has been derived from data from the SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 , MIRAS (SMOS) and SMAP satellite instruments."
            }
        },
        {
            "ob_id": 12430,
            "platform": {
                "ob_id": 29941,
                "uuid": "2b126b39dbb64c0681f12b68f2308fee",
                "short_code": "plat",
                "title": "SMAP",
                "abstract": "The Soil Moisture Active-Passive (SMAP) satelliteis a NASA satellite launched in 2015."
            },
            "instrument": {
                "ob_id": 29938,
                "uuid": "e050ad22e3b943f9a5f1563a1e6fb82c",
                "short_code": "instr",
                "title": "SMAP",
                "abstract": "The Soil Moisture Active Passive instrument is a microwave radiometer flown on the NASA SMAP satellite."
            },
            "relatedTo": {
                "ob_id": 32013,
                "uuid": "99251b53c2e84901b4bf6ec6fd78ad51",
                "short_code": "acq",
                "title": "Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v5.2",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2, MIRAS (SMOS) and SMAP)"
            }
        },
        {
            "ob_id": 12431,
            "platform": {
                "ob_id": 28095,
                "uuid": "2d34269b1f1b45c785724a912989be90",
                "short_code": "plat",
                "title": "Chulabhorn Research Institute Building, Lak Si",
                "abstract": "Chulabhorn Research Institute is a biomedical and chemistry research institute in Bangkok, Thailand."
            },
            "instrument": {
                "ob_id": 28094,
                "uuid": "95119f0a3b1f4c0bb0846b3dd08055d0",
                "short_code": "instr",
                "title": "University of Bristol: Sven Leckel LVS3",
                "abstract": "Sven Leckel LVS3 is a particle sampler."
            },
            "relatedTo": {
                "ob_id": 32042,
                "uuid": "59763d6737c849a083331cc47b69dee8",
                "short_code": "acq",
                "title": "Ultrafine and Submicron Particles in the Urban Environment in Thailand: PM10 concentration and composition measurements in Lak Si, Bangkok, Thailand",
                "abstract": "Ultrafine and Submicron Particles in the Urban Environment in Thailand: PM10 concentration and composition measurements in Lak Si, Bangkok, Thailand"
            }
        },
        {
            "ob_id": 12432,
            "platform": {
                "ob_id": 28095,
                "uuid": "2d34269b1f1b45c785724a912989be90",
                "short_code": "plat",
                "title": "Chulabhorn Research Institute Building, Lak Si",
                "abstract": "Chulabhorn Research Institute is a biomedical and chemistry research institute in Bangkok, Thailand."
            },
            "instrument": {
                "ob_id": 32045,
                "uuid": "41ed782cf88d42a0a5c4bacd5e4f564e",
                "short_code": "instr",
                "title": "University of Bristol: Dekati ELPI Classic",
                "abstract": "SDekati Electrical Low Pressure Impactor, serial number 24413"
            },
            "relatedTo": {
                "ob_id": 32046,
                "uuid": "8485b88833e84e8f8b05061c161e549b",
                "short_code": "acq",
                "title": "Ultrafine and Submicron Particles in the Urban Environment in Thailand: Aerosol concentration and composition size distributions in four locations near Bangkok, Thailand",
                "abstract": "Ultrafine and Submicron Particles in the Urban Environment in Thailand: Aerosol concentration and composition size distributions in four locations near Bangkok, Thailand"
            }
        },
        {
            "ob_id": 12433,
            "platform": {
                "ob_id": 24927,
                "uuid": "a8aa0f0e0a0745eb900bd41c37592212",
                "short_code": "plat",
                "title": "Swedish Maritime Administration Icebreaker Oden",
                "abstract": "The polar classed Icebreaker Oden (call sign SMLQ) is designed as a combined escort icebreaker and research vessel. She was the first non-nuclear icebreaker at the North Pole in 1991, with a total of seven visits. Between the years 2006-2011 she conducted five successful cruises to Antarctica. In the course of time, Oden has been upgraded and fitted with advanced scientific equipment. It was also deployed during the 2014 Arctic Cloud Summer Expedition (ACSE)."
            },
            "instrument": {
                "ob_id": 24939,
                "uuid": "6c0c95b6607e4e7dbad406a34a431fc6",
                "short_code": "instr",
                "title": "University of Leeds: Metek USA-100 sonic anemometer",
                "abstract": "The University of Leeds Metek USA-100 sonic anemometer measures turbulent winds and sonic temperature at 20Hz. 20Hz raw data are available from which average fluxes (e.g. 20 minute average fluxes) can be calculated."
            },
            "relatedTo": {
                "ob_id": 32080,
                "uuid": "106bed3e19394ca5ace4f89785109cb7",
                "short_code": "acq",
                "title": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe",
                "abstract": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe"
            }
        },
        {
            "ob_id": 12434,
            "platform": {
                "ob_id": 24927,
                "uuid": "a8aa0f0e0a0745eb900bd41c37592212",
                "short_code": "plat",
                "title": "Swedish Maritime Administration Icebreaker Oden",
                "abstract": "The polar classed Icebreaker Oden (call sign SMLQ) is designed as a combined escort icebreaker and research vessel. She was the first non-nuclear icebreaker at the North Pole in 1991, with a total of seven visits. Between the years 2006-2011 she conducted five successful cruises to Antarctica. In the course of time, Oden has been upgraded and fitted with advanced scientific equipment. It was also deployed during the 2014 Arctic Cloud Summer Expedition (ACSE)."
            },
            "instrument": {
                "ob_id": 32075,
                "uuid": "95cde815f01a4e648778c92d8b807e03",
                "short_code": "instr",
                "title": "Vaisala HMP110 temperature and humidity probe",
                "abstract": "Vaisala HMP110 temperature and humidity probe"
            },
            "relatedTo": {
                "ob_id": 32080,
                "uuid": "106bed3e19394ca5ace4f89785109cb7",
                "short_code": "acq",
                "title": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe",
                "abstract": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe"
            }
        },
        {
            "ob_id": 12435,
            "platform": {
                "ob_id": 24927,
                "uuid": "a8aa0f0e0a0745eb900bd41c37592212",
                "short_code": "plat",
                "title": "Swedish Maritime Administration Icebreaker Oden",
                "abstract": "The polar classed Icebreaker Oden (call sign SMLQ) is designed as a combined escort icebreaker and research vessel. She was the first non-nuclear icebreaker at the North Pole in 1991, with a total of seven visits. Between the years 2006-2011 she conducted five successful cruises to Antarctica. In the course of time, Oden has been upgraded and fitted with advanced scientific equipment. It was also deployed during the 2014 Arctic Cloud Summer Expedition (ACSE)."
            },
            "instrument": {
                "ob_id": 32076,
                "uuid": "add5d79c4c1049d6bfdcd6c5c7de2e82",
                "short_code": "instr",
                "title": "T-type thermocouples",
                "abstract": "The Type T is a very stable thermocouple and is often used in extremely low temperature applications such as cryogenics or ultra low freezers."
            },
            "relatedTo": {
                "ob_id": 32080,
                "uuid": "106bed3e19394ca5ace4f89785109cb7",
                "short_code": "acq",
                "title": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe",
                "abstract": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe"
            }
        },
        {
            "ob_id": 12436,
            "platform": {
                "ob_id": 24927,
                "uuid": "a8aa0f0e0a0745eb900bd41c37592212",
                "short_code": "plat",
                "title": "Swedish Maritime Administration Icebreaker Oden",
                "abstract": "The polar classed Icebreaker Oden (call sign SMLQ) is designed as a combined escort icebreaker and research vessel. She was the first non-nuclear icebreaker at the North Pole in 1991, with a total of seven visits. Between the years 2006-2011 she conducted five successful cruises to Antarctica. In the course of time, Oden has been upgraded and fitted with advanced scientific equipment. It was also deployed during the 2014 Arctic Cloud Summer Expedition (ACSE)."
            },
            "instrument": {
                "ob_id": 32077,
                "uuid": "b61381027bbb432185707e3b6d20a14d",
                "short_code": "instr",
                "title": "NRG Type 40 cupanemometers",
                "abstract": "NRG Type 40 cupanemometers measures wind speed."
            },
            "relatedTo": {
                "ob_id": 32080,
                "uuid": "106bed3e19394ca5ace4f89785109cb7",
                "short_code": "acq",
                "title": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe",
                "abstract": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe"
            }
        },
        {
            "ob_id": 12437,
            "platform": {
                "ob_id": 24927,
                "uuid": "a8aa0f0e0a0745eb900bd41c37592212",
                "short_code": "plat",
                "title": "Swedish Maritime Administration Icebreaker Oden",
                "abstract": "The polar classed Icebreaker Oden (call sign SMLQ) is designed as a combined escort icebreaker and research vessel. She was the first non-nuclear icebreaker at the North Pole in 1991, with a total of seven visits. Between the years 2006-2011 she conducted five successful cruises to Antarctica. In the course of time, Oden has been upgraded and fitted with advanced scientific equipment. It was also deployed during the 2014 Arctic Cloud Summer Expedition (ACSE)."
            },
            "instrument": {
                "ob_id": 32078,
                "uuid": "e66f3221c2b34cb3ac4e9d09676a02a5",
                "short_code": "instr",
                "title": "Kipp & Zonen CMP22 pyranometer",
                "abstract": "Kipp & Zonen CMP22 pyranometer measures solar irradiance on a planar surface."
            },
            "relatedTo": {
                "ob_id": 32080,
                "uuid": "106bed3e19394ca5ace4f89785109cb7",
                "short_code": "acq",
                "title": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe",
                "abstract": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe"
            }
        },
        {
            "ob_id": 12438,
            "platform": {
                "ob_id": 24927,
                "uuid": "a8aa0f0e0a0745eb900bd41c37592212",
                "short_code": "plat",
                "title": "Swedish Maritime Administration Icebreaker Oden",
                "abstract": "The polar classed Icebreaker Oden (call sign SMLQ) is designed as a combined escort icebreaker and research vessel. She was the first non-nuclear icebreaker at the North Pole in 1991, with a total of seven visits. Between the years 2006-2011 she conducted five successful cruises to Antarctica. In the course of time, Oden has been upgraded and fitted with advanced scientific equipment. It was also deployed during the 2014 Arctic Cloud Summer Expedition (ACSE)."
            },
            "instrument": {
                "ob_id": 32079,
                "uuid": "dda133ffd5f24a20a839450a2059ac4b",
                "short_code": "instr",
                "title": "CGR4 pyrgeometer",
                "abstract": "CGR4 pyrgeometer measures solar radiance."
            },
            "relatedTo": {
                "ob_id": 32080,
                "uuid": "106bed3e19394ca5ace4f89785109cb7",
                "short_code": "acq",
                "title": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe",
                "abstract": "Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): Meteorological data from the measurement station on the ice floe"
            }
        }
    ]
}