Instrument Platform Pair List

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    "count": 14115,
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    "results": [
        {
            "ob_id": 11205,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 8621,
                "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                "short_code": "instr",
                "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
            },
            "relatedTo": {
                "ob_id": 24640,
                "uuid": "fef8a337c2cc49268ae7564b2fe3a251",
                "short_code": "acq",
                "title": "ARSF 2015_169a - EUFAR MEDHY2CON/EUFAR15_38 Flight: data acquisition details",
                "abstract": "ARSF 2015_169a - EUFAR MEDHY2CON/EUFAR15_38 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11206,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 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": 24645,
                "uuid": "883a47da184241909d426e037ef4e95a",
                "short_code": "acq",
                "title": "ARSF 2015_169b - EUFAR MEDHY2CON/EUFAR15_38 Flight: data acquisition details",
                "abstract": "ARSF 2015_169b - EUFAR MEDHY2CON/EUFAR15_38 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11207,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 8621,
                "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                "short_code": "instr",
                "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
            },
            "relatedTo": {
                "ob_id": 24645,
                "uuid": "883a47da184241909d426e037ef4e95a",
                "short_code": "acq",
                "title": "ARSF 2015_169b - EUFAR MEDHY2CON/EUFAR15_38 Flight: data acquisition details",
                "abstract": "ARSF 2015_169b - EUFAR MEDHY2CON/EUFAR15_38 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11208,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 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": 24649,
                "uuid": "7767b35142a0466f9d8105ecd2397e2a",
                "short_code": "acq",
                "title": "ARSF 2015_170 - EUFAR MEDHY2CON/EUFAR15_38 Flight: data acquisition details",
                "abstract": "ARSF 2015_170 - EUFAR MEDHY2CON/EUFAR15_38 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11209,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 8621,
                "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                "short_code": "instr",
                "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
            },
            "relatedTo": {
                "ob_id": 24649,
                "uuid": "7767b35142a0466f9d8105ecd2397e2a",
                "short_code": "acq",
                "title": "ARSF 2015_170 - EUFAR MEDHY2CON/EUFAR15_38 Flight: data acquisition details",
                "abstract": "ARSF 2015_170 - EUFAR MEDHY2CON/EUFAR15_38 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11210,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 10202,
                "uuid": "4ba81218ece24bb89ed01d615e39be05",
                "short_code": "instr",
                "title": "ARSF Rollei Digital Camera",
                "abstract": "The ARSF ROLLEI digital camera is used to obtain imagery at the same time as the other instruments.  This camera replaces the previous film format Wild RC series cameras(?)"
            },
            "relatedTo": {
                "ob_id": 24653,
                "uuid": "f3be325e35144cc68fe80f18ebd781e8",
                "short_code": "acq",
                "title": "ARSF 2015_268 - EUFAR MEDHY2CON/EUFAR15_38 Flight: data acquisition details",
                "abstract": "ARSF 2015_268 - EUFAR MEDHY2CON/EUFAR15_38 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11211,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 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": 24653,
                "uuid": "f3be325e35144cc68fe80f18ebd781e8",
                "short_code": "acq",
                "title": "ARSF 2015_268 - EUFAR MEDHY2CON/EUFAR15_38 Flight: data acquisition details",
                "abstract": "ARSF 2015_268 - EUFAR MEDHY2CON/EUFAR15_38 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11212,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 8621,
                "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                "short_code": "instr",
                "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
            },
            "relatedTo": {
                "ob_id": 24653,
                "uuid": "f3be325e35144cc68fe80f18ebd781e8",
                "short_code": "acq",
                "title": "ARSF 2015_268 - EUFAR MEDHY2CON/EUFAR15_38 Flight: data acquisition details",
                "abstract": "ARSF 2015_268 - EUFAR MEDHY2CON/EUFAR15_38 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11213,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 8621,
                "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                "short_code": "instr",
                "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
            },
            "relatedTo": {
                "ob_id": 24657,
                "uuid": "c582f07d7df6430a92269815e74a63a4",
                "short_code": "acq",
                "title": "ARSF 2015_174 - EUFAR AHSPECT/EUFAR15_18 Flight: data acquisition details",
                "abstract": "ARSF 2015_174 - EUFAR AHSPECT/EUFAR15_18 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11214,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 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": 24657,
                "uuid": "c582f07d7df6430a92269815e74a63a4",
                "short_code": "acq",
                "title": "ARSF 2015_174 - EUFAR AHSPECT/EUFAR15_18 Flight: data acquisition details",
                "abstract": "ARSF 2015_174 - EUFAR AHSPECT/EUFAR15_18 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11215,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 10202,
                "uuid": "4ba81218ece24bb89ed01d615e39be05",
                "short_code": "instr",
                "title": "ARSF Rollei Digital Camera",
                "abstract": "The ARSF ROLLEI digital camera is used to obtain imagery at the same time as the other instruments.  This camera replaces the previous film format Wild RC series cameras(?)"
            },
            "relatedTo": {
                "ob_id": 24662,
                "uuid": "35e69e19d12046529c36fd808e4091b7",
                "short_code": "acq",
                "title": "ARSF 2015_274 - EUFAR AHSPECT/EUFAR15_18 Flight: data acquisition details",
                "abstract": "ARSF 2015_274 - EUFAR AHSPECT/EUFAR15_18 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11216,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 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": 24662,
                "uuid": "35e69e19d12046529c36fd808e4091b7",
                "short_code": "acq",
                "title": "ARSF 2015_274 - EUFAR AHSPECT/EUFAR15_18 Flight: data acquisition details",
                "abstract": "ARSF 2015_274 - EUFAR AHSPECT/EUFAR15_18 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11217,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 8621,
                "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                "short_code": "instr",
                "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
            },
            "relatedTo": {
                "ob_id": 24662,
                "uuid": "35e69e19d12046529c36fd808e4091b7",
                "short_code": "acq",
                "title": "ARSF 2015_274 - EUFAR AHSPECT/EUFAR15_18 Flight: data acquisition details",
                "abstract": "ARSF 2015_274 - EUFAR AHSPECT/EUFAR15_18 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11218,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 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": 24666,
                "uuid": "238331f6c6f74bfa97c73800821d20ce",
                "short_code": "acq",
                "title": "ARSF 2015_175a - EUFAR ISOTHERM/EUFAR15_28 Flight: data acquisition details",
                "abstract": "ARSF 2015_175a - EUFAR ISOTHERM/EUFAR15_28 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11219,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 8621,
                "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                "short_code": "instr",
                "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
            },
            "relatedTo": {
                "ob_id": 24666,
                "uuid": "238331f6c6f74bfa97c73800821d20ce",
                "short_code": "acq",
                "title": "ARSF 2015_175a - EUFAR ISOTHERM/EUFAR15_28 Flight: data acquisition details",
                "abstract": "ARSF 2015_175a - EUFAR ISOTHERM/EUFAR15_28 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11220,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 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": 24671,
                "uuid": "f2e6be7582cd4ac49d8ac3bcb7eb2f8a",
                "short_code": "acq",
                "title": "ARSF 2015_175b - EUFAR ISOTHERM/EUFAR15_28 Flight: data acquisition details",
                "abstract": "ARSF 2015_175b - EUFAR ISOTHERM/EUFAR15_28 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11221,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 8621,
                "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                "short_code": "instr",
                "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
            },
            "relatedTo": {
                "ob_id": 24671,
                "uuid": "f2e6be7582cd4ac49d8ac3bcb7eb2f8a",
                "short_code": "acq",
                "title": "ARSF 2015_175b - EUFAR ISOTHERM/EUFAR15_28 Flight: data acquisition details",
                "abstract": "ARSF 2015_175b - EUFAR ISOTHERM/EUFAR15_28 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11222,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 10202,
                "uuid": "4ba81218ece24bb89ed01d615e39be05",
                "short_code": "instr",
                "title": "ARSF Rollei Digital Camera",
                "abstract": "The ARSF ROLLEI digital camera is used to obtain imagery at the same time as the other instruments.  This camera replaces the previous film format Wild RC series cameras(?)"
            },
            "relatedTo": {
                "ob_id": 24675,
                "uuid": "371dbaef94804601acf67e4de79a1f92",
                "short_code": "acq",
                "title": "ARSF 2015_271a - EUFAR ISOTHERM/EUFAR15_28 Flight: data acquisition details",
                "abstract": "ARSF 2015_271a - EUFAR ISOTHERM/EUFAR15_28 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11223,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 8621,
                "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                "short_code": "instr",
                "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
            },
            "relatedTo": {
                "ob_id": 24675,
                "uuid": "371dbaef94804601acf67e4de79a1f92",
                "short_code": "acq",
                "title": "ARSF 2015_271a - EUFAR ISOTHERM/EUFAR15_28 Flight: data acquisition details",
                "abstract": "ARSF 2015_271a - EUFAR ISOTHERM/EUFAR15_28 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11224,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 10202,
                "uuid": "4ba81218ece24bb89ed01d615e39be05",
                "short_code": "instr",
                "title": "ARSF Rollei Digital Camera",
                "abstract": "The ARSF ROLLEI digital camera is used to obtain imagery at the same time as the other instruments.  This camera replaces the previous film format Wild RC series cameras(?)"
            },
            "relatedTo": {
                "ob_id": 24679,
                "uuid": "54f384bd8dbd42ffbd1a74ee336050b6",
                "short_code": "acq",
                "title": "ARSF 2015_271b - EUFAR ISOTHERM/EUFAR15_28 Flight: data acquisition details",
                "abstract": "ARSF 2015_271b - EUFAR ISOTHERM/EUFAR15_28 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11225,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 8621,
                "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                "short_code": "instr",
                "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
            },
            "relatedTo": {
                "ob_id": 24679,
                "uuid": "54f384bd8dbd42ffbd1a74ee336050b6",
                "short_code": "acq",
                "title": "ARSF 2015_271b - EUFAR ISOTHERM/EUFAR15_28 Flight: data acquisition details",
                "abstract": "ARSF 2015_271b - EUFAR ISOTHERM/EUFAR15_28 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11226,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 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": 24679,
                "uuid": "54f384bd8dbd42ffbd1a74ee336050b6",
                "short_code": "acq",
                "title": "ARSF 2015_271b - EUFAR ISOTHERM/EUFAR15_28 Flight: data acquisition details",
                "abstract": "ARSF 2015_271b - EUFAR ISOTHERM/EUFAR15_28 Flight data acquisition details."
            }
        },
        {
            "ob_id": 11227,
            "platform": {
                "ob_id": 24683,
                "uuid": "71c3e8ee302943c78642e414e6fbd03b",
                "short_code": "plat",
                "title": "Fennec automatic weather station (AWS) network",
                "abstract": "The Fennec automatic weather station (AWS) network consists of eight stations installed across the Sahara, with four in remote locations in the central desert, where no previous meteorological observations have existed previously. They were operated autonomously starting in Summer 2011, with some stations continuing to produce data into 2013. Data were transmitted via satellite link to the University of Leeds.\r\n\r\nA data information sheet has been supplied with data files and is available via CEDA. A description of the AWS network is included as part of Hobby et al., (2013). \r\n\r\nIndividual AWS locations as follows:\r\nStation 131 (Blue) - 24.280 N 2.136 W\r\n\r\nStation 133 (Yellow) - 25.374 N 5.786 W\r\n\r\nStation 134 (Black) - 23.500 N 2.990 W\r\n\r\nStation 135 (White) - 23.480 N 7.843 W\r\n\r\nStation 136_1 (Tamanrasset) - 22.785 N 5.522 E\r\n\r\nStation 136_2 (Bordj Badji Mokhtar) - 21.325 N 0.946 E\r\n\r\nStation 138 (Grey) - 27.370 N 3.018 W\r\n\r\nStation 140 (Orange) - 26.053 N 4.221 W\r\n\r\nStation 141 (Purple) - 25.227 N 11.578 W"
            },
            "instrument": {
                "ob_id": 24684,
                "uuid": "9073e6518bd845ffa9e5b26a0480dd2b",
                "short_code": "instr",
                "title": "Fennec automatic weather station",
                "abstract": "Automatic weather stations (AWSs) were deployed at 8 stations in the Sahara in 2011 (until 2013 for some stations) as part of the Fennec field campaign. \r\n\r\nDesigned and built at the University of Leeds they include: \r\nIntersema MS55634 pressure sensors, Mierij Meteo MW36 cup anemometers, Vaisala WMT52 sonic anemometers, Epluse EE08 temperature and relative humidity sensors, Omega 44007 thermistors, Hukseflux HFP01SC ground flux sensor and Kipp & Zonen CNR4 radiometers. \r\n\r\nFor more information on the construction of the AWSs please see Hobby et al., (2013). "
            },
            "relatedTo": null
        },
        {
            "ob_id": 11228,
            "platform": {
                "ob_id": 24683,
                "uuid": "71c3e8ee302943c78642e414e6fbd03b",
                "short_code": "plat",
                "title": "Fennec automatic weather station (AWS) network",
                "abstract": "The Fennec automatic weather station (AWS) network consists of eight stations installed across the Sahara, with four in remote locations in the central desert, where no previous meteorological observations have existed previously. They were operated autonomously starting in Summer 2011, with some stations continuing to produce data into 2013. Data were transmitted via satellite link to the University of Leeds.\r\n\r\nA data information sheet has been supplied with data files and is available via CEDA. A description of the AWS network is included as part of Hobby et al., (2013). \r\n\r\nIndividual AWS locations as follows:\r\nStation 131 (Blue) - 24.280 N 2.136 W\r\n\r\nStation 133 (Yellow) - 25.374 N 5.786 W\r\n\r\nStation 134 (Black) - 23.500 N 2.990 W\r\n\r\nStation 135 (White) - 23.480 N 7.843 W\r\n\r\nStation 136_1 (Tamanrasset) - 22.785 N 5.522 E\r\n\r\nStation 136_2 (Bordj Badji Mokhtar) - 21.325 N 0.946 E\r\n\r\nStation 138 (Grey) - 27.370 N 3.018 W\r\n\r\nStation 140 (Orange) - 26.053 N 4.221 W\r\n\r\nStation 141 (Purple) - 25.227 N 11.578 W"
            },
            "instrument": {
                "ob_id": 24684,
                "uuid": "9073e6518bd845ffa9e5b26a0480dd2b",
                "short_code": "instr",
                "title": "Fennec automatic weather station",
                "abstract": "Automatic weather stations (AWSs) were deployed at 8 stations in the Sahara in 2011 (until 2013 for some stations) as part of the Fennec field campaign. \r\n\r\nDesigned and built at the University of Leeds they include: \r\nIntersema MS55634 pressure sensors, Mierij Meteo MW36 cup anemometers, Vaisala WMT52 sonic anemometers, Epluse EE08 temperature and relative humidity sensors, Omega 44007 thermistors, Hukseflux HFP01SC ground flux sensor and Kipp & Zonen CNR4 radiometers. \r\n\r\nFor more information on the construction of the AWSs please see Hobby et al., (2013). "
            },
            "relatedTo": {
                "ob_id": 24690,
                "uuid": "bc467943f03141dea0edd8606b597e82",
                "short_code": "acq",
                "title": "Acquisition for Fennec station data",
                "abstract": "Data were acquired from 8 stations in the Sahara between 2011-2013 via Automatic Weather Stations (AWS)"
            }
        },
        {
            "ob_id": 11229,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
            "relatedTo": {
                "ob_id": 24721,
                "uuid": "6a6083a9b17d449b84e1440a9078a2fd",
                "short_code": "acq",
                "title": "FAAM Flight B992 Acquisition",
                "abstract": "FAAM Flight B992 Acquisition"
            }
        },
        {
            "ob_id": 11230,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 5799,
                "uuid": "c7e2a6a5c6204b09ac3a5c266752ca9c",
                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
            "relatedTo": {
                "ob_id": 24721,
                "uuid": "6a6083a9b17d449b84e1440a9078a2fd",
                "short_code": "acq",
                "title": "FAAM Flight B992 Acquisition",
                "abstract": "FAAM Flight B992 Acquisition"
            }
        },
        {
            "ob_id": 11231,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
            },
            "relatedTo": {
                "ob_id": 24721,
                "uuid": "6a6083a9b17d449b84e1440a9078a2fd",
                "short_code": "acq",
                "title": "FAAM Flight B992 Acquisition",
                "abstract": "FAAM Flight B992 Acquisition"
            }
        },
        {
            "ob_id": 11232,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
            "relatedTo": {
                "ob_id": 24725,
                "uuid": "98c767086a1c4bf4867384381f58ad01",
                "short_code": "acq",
                "title": "FAAM Flight B993 Acquisition",
                "abstract": "FAAM Flight B993 Acquisition"
            }
        },
        {
            "ob_id": 11233,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 5799,
                "uuid": "c7e2a6a5c6204b09ac3a5c266752ca9c",
                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
            "relatedTo": {
                "ob_id": 24725,
                "uuid": "98c767086a1c4bf4867384381f58ad01",
                "short_code": "acq",
                "title": "FAAM Flight B993 Acquisition",
                "abstract": "FAAM Flight B993 Acquisition"
            }
        },
        {
            "ob_id": 11234,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
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                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
            },
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                "uuid": "98c767086a1c4bf4867384381f58ad01",
                "short_code": "acq",
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                "abstract": "FAAM Flight B993 Acquisition"
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
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                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
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                "ob_id": 24729,
                "uuid": "456c65dd7e5e492d8783377644c3062d",
                "short_code": "acq",
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
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                "short_code": "instr",
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                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
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                "ob_id": 24729,
                "uuid": "456c65dd7e5e492d8783377644c3062d",
                "short_code": "acq",
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
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                "uuid": "ca3c48564db10ffbdfe37264a4ff16fd",
                "short_code": "instr",
                "title": "FAAM Fast Greenhouse Gas analyser",
                "abstract": "FAAM Fast Greenhouse Gas analyser. FAAM non-core instrument first used in BORTAS project."
            },
            "relatedTo": {
                "ob_id": 24729,
                "uuid": "456c65dd7e5e492d8783377644c3062d",
                "short_code": "acq",
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        {
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            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
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                "ob_id": 24729,
                "uuid": "456c65dd7e5e492d8783377644c3062d",
                "short_code": "acq",
                "title": "FAAM Flight B994 Acquisition",
                "abstract": "FAAM Flight B994 Acquisition"
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
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                "uuid": "97b8455f0ffb46fbb55b0d2d696700ad",
                "short_code": "acq",
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        {
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "uuid": "c7e2a6a5c6204b09ac3a5c266752ca9c",
                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
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                "uuid": "97b8455f0ffb46fbb55b0d2d696700ad",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "uuid": "ca3c48564db10ffbdfe37264a4ff16fd",
                "short_code": "instr",
                "title": "FAAM Fast Greenhouse Gas analyser",
                "abstract": "FAAM Fast Greenhouse Gas analyser. FAAM non-core instrument first used in BORTAS project."
            },
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                "ob_id": 24733,
                "uuid": "97b8455f0ffb46fbb55b0d2d696700ad",
                "short_code": "acq",
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        {
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
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                "uuid": "de1af665fddd47d599eb2eee7ebeddde",
                "short_code": "acq",
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "abstract": "Instrument.abstract: DETAILS NEEDED"
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                "uuid": "de1af665fddd47d599eb2eee7ebeddde",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "short_code": "acq",
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                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "abstract": "Instrument.abstract: DETAILS NEEDED"
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                "uuid": "122b4f66bbe141faab99120a155abcfd",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "uuid": "122b4f66bbe141faab99120a155abcfd",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "short_code": "instr",
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                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
            },
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                "short_code": "acq",
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                "abstract": "FAAM Flight B997 Acquisition"
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
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                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
            "relatedTo": {
                "ob_id": 24746,
                "uuid": "312cf3cff7be45a389f5393d813db15f",
                "short_code": "acq",
                "title": "FAAM Flight B998 Acquisition",
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            }
        },
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
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                "uuid": "c7e2a6a5c6204b09ac3a5c266752ca9c",
                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
            "relatedTo": {
                "ob_id": 24746,
                "uuid": "312cf3cff7be45a389f5393d813db15f",
                "short_code": "acq",
                "title": "FAAM Flight B998 Acquisition",
                "abstract": "FAAM Flight B998 Acquisition"
            }
        },
        {
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 11730,
                "uuid": "ca3c48564db10ffbdfe37264a4ff16fd",
                "short_code": "instr",
                "title": "FAAM Fast Greenhouse Gas analyser",
                "abstract": "FAAM Fast Greenhouse Gas analyser. FAAM non-core instrument first used in BORTAS project."
            },
            "relatedTo": {
                "ob_id": 24746,
                "uuid": "312cf3cff7be45a389f5393d813db15f",
                "short_code": "acq",
                "title": "FAAM Flight B998 Acquisition",
                "abstract": "FAAM Flight B998 Acquisition"
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        },
        {
            "ob_id": 11253,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
            },
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                "ob_id": 24746,
                "uuid": "312cf3cff7be45a389f5393d813db15f",
                "short_code": "acq",
                "title": "FAAM Flight B998 Acquisition",
                "abstract": "FAAM Flight B998 Acquisition"
            }
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            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
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                "ob_id": 24750,
                "uuid": "7ae8b5122030405692a7c2b3c27b14e7",
                "short_code": "acq",
                "title": "FAAM Flight B999 Acquisition",
                "abstract": "FAAM Flight B999 Acquisition"
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        {
            "ob_id": 11255,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
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                "uuid": "c7e2a6a5c6204b09ac3a5c266752ca9c",
                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
            "relatedTo": {
                "ob_id": 24750,
                "uuid": "7ae8b5122030405692a7c2b3c27b14e7",
                "short_code": "acq",
                "title": "FAAM Flight B999 Acquisition",
                "abstract": "FAAM Flight B999 Acquisition"
            }
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        {
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
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                "uuid": "ca3c48564db10ffbdfe37264a4ff16fd",
                "short_code": "instr",
                "title": "FAAM Fast Greenhouse Gas analyser",
                "abstract": "FAAM Fast Greenhouse Gas analyser. FAAM non-core instrument first used in BORTAS project."
            },
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                "ob_id": 24750,
                "uuid": "7ae8b5122030405692a7c2b3c27b14e7",
                "short_code": "acq",
                "title": "FAAM Flight B999 Acquisition",
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        {
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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            "instrument": {
                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
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                "ob_id": 24750,
                "uuid": "7ae8b5122030405692a7c2b3c27b14e7",
                "short_code": "acq",
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                "abstract": "FAAM Flight B999 Acquisition"
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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            "instrument": {
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                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
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                "ob_id": 24754,
                "uuid": "b46567cb681e424fad94785bdc454b46",
                "short_code": "acq",
                "title": "FAAM Flight C001 Acquisition",
                "abstract": "FAAM Flight C001 Acquisition"
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
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                "ob_id": 24754,
                "uuid": "b46567cb681e424fad94785bdc454b46",
                "short_code": "acq",
                "title": "FAAM Flight C001 Acquisition",
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        {
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                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "short_code": "instr",
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                "abstract": "FAAM Fast Greenhouse Gas analyser. FAAM non-core instrument first used in BORTAS project."
            },
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                "uuid": "b46567cb681e424fad94785bdc454b46",
                "short_code": "acq",
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                "uuid": "dda4596d5d374564acf8c79b7a119127",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
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                "uuid": "b46567cb681e424fad94785bdc454b46",
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
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                "uuid": "ac488ef2a4674c2ab2cc079f60e0dcaf",
                "short_code": "acq",
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                "abstract": "FAAM Flight C002 Acquisition"
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                "uuid": "dda4596d5d374564acf8c79b7a119127",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "uuid": "c7e2a6a5c6204b09ac3a5c266752ca9c",
                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
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                "uuid": "ac488ef2a4674c2ab2cc079f60e0dcaf",
                "short_code": "acq",
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                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
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                "short_code": "instr",
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                "uuid": "ac488ef2a4674c2ab2cc079f60e0dcaf",
                "short_code": "acq",
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                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
            },
            "relatedTo": {
                "ob_id": 24758,
                "uuid": "ac488ef2a4674c2ab2cc079f60e0dcaf",
                "short_code": "acq",
                "title": "FAAM Flight C002 Acquisition",
                "abstract": "FAAM Flight C002 Acquisition"
            }
        },
        {
            "ob_id": 11266,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
            "relatedTo": {
                "ob_id": 24763,
                "uuid": "80cfc38bb3434b0e9572af5a84a91bfe",
                "short_code": "acq",
                "title": "FAAM Flight C003 Acquisition",
                "abstract": "FAAM Flight C003 Acquisition"
            }
        },
        {
            "ob_id": 11267,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 11730,
                "uuid": "ca3c48564db10ffbdfe37264a4ff16fd",
                "short_code": "instr",
                "title": "FAAM Fast Greenhouse Gas analyser",
                "abstract": "FAAM Fast Greenhouse Gas analyser. FAAM non-core instrument first used in BORTAS project."
            },
            "relatedTo": {
                "ob_id": 24763,
                "uuid": "80cfc38bb3434b0e9572af5a84a91bfe",
                "short_code": "acq",
                "title": "FAAM Flight C003 Acquisition",
                "abstract": "FAAM Flight C003 Acquisition"
            }
        },
        {
            "ob_id": 11268,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
            "relatedTo": {
                "ob_id": 24767,
                "uuid": "01626973fa884a8abf91fdb9e04f08fe",
                "short_code": "acq",
                "title": "FAAM Flight C004 Acquisition",
                "abstract": "FAAM Flight C004 Acquisition"
            }
        },
        {
            "ob_id": 11269,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 11730,
                "uuid": "ca3c48564db10ffbdfe37264a4ff16fd",
                "short_code": "instr",
                "title": "FAAM Fast Greenhouse Gas analyser",
                "abstract": "FAAM Fast Greenhouse Gas analyser. FAAM non-core instrument first used in BORTAS project."
            },
            "relatedTo": {
                "ob_id": 24767,
                "uuid": "01626973fa884a8abf91fdb9e04f08fe",
                "short_code": "acq",
                "title": "FAAM Flight C004 Acquisition",
                "abstract": "FAAM Flight C004 Acquisition"
            }
        },
        {
            "ob_id": 11270,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
            "relatedTo": {
                "ob_id": 24771,
                "uuid": "158b3fb22d8b4fc3876c9960d4b7dd20",
                "short_code": "acq",
                "title": "FAAM Flight C005 Acquisition",
                "abstract": "FAAM Flight C005 Acquisition"
            }
        },
        {
            "ob_id": 11271,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 11730,
                "uuid": "ca3c48564db10ffbdfe37264a4ff16fd",
                "short_code": "instr",
                "title": "FAAM Fast Greenhouse Gas analyser",
                "abstract": "FAAM Fast Greenhouse Gas analyser. FAAM non-core instrument first used in BORTAS project."
            },
            "relatedTo": {
                "ob_id": 24771,
                "uuid": "158b3fb22d8b4fc3876c9960d4b7dd20",
                "short_code": "acq",
                "title": "FAAM Flight C005 Acquisition",
                "abstract": "FAAM Flight C005 Acquisition"
            }
        },
        {
            "ob_id": 11272,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
            "relatedTo": {
                "ob_id": 24775,
                "uuid": "9e76e955a56c4f2ea939321af7c5b6d5",
                "short_code": "acq",
                "title": "FAAM Flight C006 Acquisition",
                "abstract": "FAAM Flight C006 Acquisition"
            }
        },
        {
            "ob_id": 11273,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 11730,
                "uuid": "ca3c48564db10ffbdfe37264a4ff16fd",
                "short_code": "instr",
                "title": "FAAM Fast Greenhouse Gas analyser",
                "abstract": "FAAM Fast Greenhouse Gas analyser. FAAM non-core instrument first used in BORTAS project."
            },
            "relatedTo": {
                "ob_id": 24775,
                "uuid": "9e76e955a56c4f2ea939321af7c5b6d5",
                "short_code": "acq",
                "title": "FAAM Flight C006 Acquisition",
                "abstract": "FAAM Flight C006 Acquisition"
            }
        },
        {
            "ob_id": 11274,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
            "relatedTo": {
                "ob_id": 24779,
                "uuid": "65372f93cdf646b082cd16785e743e3f",
                "short_code": "acq",
                "title": "FAAM Flight C007 Acquisition",
                "abstract": "FAAM Flight C007 Acquisition"
            }
        },
        {
            "ob_id": 11275,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 11730,
                "uuid": "ca3c48564db10ffbdfe37264a4ff16fd",
                "short_code": "instr",
                "title": "FAAM Fast Greenhouse Gas analyser",
                "abstract": "FAAM Fast Greenhouse Gas analyser. FAAM non-core instrument first used in BORTAS project."
            },
            "relatedTo": {
                "ob_id": 24779,
                "uuid": "65372f93cdf646b082cd16785e743e3f",
                "short_code": "acq",
                "title": "FAAM Flight C007 Acquisition",
                "abstract": "FAAM Flight C007 Acquisition"
            }
        },
        {
            "ob_id": 11276,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
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                "ob_id": 24783,
                "uuid": "b7e71f35b24f42e7b0b0ed19cdffb931",
                "short_code": "acq",
                "title": "FAAM Flight C008 Acquisition",
                "abstract": "FAAM Flight C008 Acquisition"
            }
        },
        {
            "ob_id": 11277,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 11730,
                "uuid": "ca3c48564db10ffbdfe37264a4ff16fd",
                "short_code": "instr",
                "title": "FAAM Fast Greenhouse Gas analyser",
                "abstract": "FAAM Fast Greenhouse Gas analyser. FAAM non-core instrument first used in BORTAS project."
            },
            "relatedTo": {
                "ob_id": 24783,
                "uuid": "b7e71f35b24f42e7b0b0ed19cdffb931",
                "short_code": "acq",
                "title": "FAAM Flight C008 Acquisition",
                "abstract": "FAAM Flight C008 Acquisition"
            }
        },
        {
            "ob_id": 11278,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
            "relatedTo": {
                "ob_id": 24787,
                "uuid": "f325db8371ac417f9d1d902d7cd0f0e3",
                "short_code": "acq",
                "title": "FAAM Flight C009 Acquisition",
                "abstract": "FAAM Flight C009 Acquisition"
            }
        },
        {
            "ob_id": 11279,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 5799,
                "uuid": "c7e2a6a5c6204b09ac3a5c266752ca9c",
                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
            "relatedTo": {
                "ob_id": 24787,
                "uuid": "f325db8371ac417f9d1d902d7cd0f0e3",
                "short_code": "acq",
                "title": "FAAM Flight C009 Acquisition",
                "abstract": "FAAM Flight C009 Acquisition"
            }
        },
        {
            "ob_id": 11280,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
            },
            "relatedTo": {
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                "uuid": "f325db8371ac417f9d1d902d7cd0f0e3",
                "short_code": "acq",
                "title": "FAAM Flight C009 Acquisition",
                "abstract": "FAAM Flight C009 Acquisition"
            }
        },
        {
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            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
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                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
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                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
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                "short_code": "acq",
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                "abstract": "FAAM Flight C010 Acquisition"
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            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
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                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
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                "ob_id": 24791,
                "uuid": "94b80a8d3c184f3b8039f7baab418922",
                "short_code": "acq",
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            }
        },
        {
            "ob_id": 11283,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
            },
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                "uuid": "94b80a8d3c184f3b8039f7baab418922",
                "short_code": "acq",
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                "abstract": "FAAM Flight C010 Acquisition"
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        {
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            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
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                "ob_id": 24795,
                "uuid": "6e57914ba5b146d9917dc7fc5cd4000e",
                "short_code": "acq",
                "title": "FAAM Flight C011 Acquisition",
                "abstract": "FAAM Flight C011 Acquisition"
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        {
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            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
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                "uuid": "c7e2a6a5c6204b09ac3a5c266752ca9c",
                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
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                "ob_id": 24795,
                "uuid": "6e57914ba5b146d9917dc7fc5cd4000e",
                "short_code": "acq",
                "title": "FAAM Flight C011 Acquisition",
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        {
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            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
            },
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                "ob_id": 24795,
                "uuid": "6e57914ba5b146d9917dc7fc5cd4000e",
                "short_code": "acq",
                "title": "FAAM Flight C011 Acquisition",
                "abstract": "FAAM Flight C011 Acquisition"
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        {
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            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
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                "ob_id": 24799,
                "uuid": "bb1ed016e2154fb3b1e868c5c2fca7a8",
                "short_code": "acq",
                "title": "FAAM Flight C012 Acquisition",
                "abstract": "FAAM Flight C012 Acquisition"
            }
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        {
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            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 5799,
                "uuid": "c7e2a6a5c6204b09ac3a5c266752ca9c",
                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
            "relatedTo": {
                "ob_id": 24799,
                "uuid": "bb1ed016e2154fb3b1e868c5c2fca7a8",
                "short_code": "acq",
                "title": "FAAM Flight C012 Acquisition",
                "abstract": "FAAM Flight C012 Acquisition"
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        {
            "ob_id": 11289,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
            },
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                "ob_id": 24799,
                "uuid": "bb1ed016e2154fb3b1e868c5c2fca7a8",
                "short_code": "acq",
                "title": "FAAM Flight C012 Acquisition",
                "abstract": "FAAM Flight C012 Acquisition"
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        {
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            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 61,
                "uuid": "306ac6a158514192baf813b4b8b46be7",
                "short_code": "instr",
                "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
            },
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                "ob_id": 24803,
                "uuid": "dea632c433ec4782a2e884e532bb22ee",
                "short_code": "acq",
                "title": "FAAM Flight C013 Acquisition",
                "abstract": "FAAM Flight C013 Acquisition"
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        {
            "ob_id": 11291,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 5799,
                "uuid": "c7e2a6a5c6204b09ac3a5c266752ca9c",
                "short_code": "instr",
                "title": "FAAM/BAE systems: Subset of FAAM core instruments measuring cloud physics data",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
            "relatedTo": {
                "ob_id": 24803,
                "uuid": "dea632c433ec4782a2e884e532bb22ee",
                "short_code": "acq",
                "title": "FAAM Flight C013 Acquisition",
                "abstract": "FAAM Flight C013 Acquisition"
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        {
            "ob_id": 11292,
            "platform": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "instrument": {
                "ob_id": 13673,
                "uuid": "fbfd40bdaea44388a7a8c0abddec37ec",
                "short_code": "instr",
                "title": "AIMMS-20 (Airborne Integrated Meteorological Measurement System)",
                "abstract": "The AIMMS-20 (Airborne Integrated Meteorological Measurement System) is a canister-mounting probe flown on the FAAM BAe-146 aircraft. Its primary purpose is to provide high-frequency measurements of 3-d wind vector components in icing conditions, where the Core radome turbulence system would be expected to ice-up. The probe comprises a 5-port differential pressure sensor to measure flow velocity relative to the aircraft (true airspeed and angles of attack/sideslip) and a combined GPS/inertial system to measure the velocity and attitude of the aircraft relative to the ground.\r\n\r\nMeteorological parameters: Temperature Relative Humidity Wind vector (3-components) Static pressure Aircraft state parameters: Latitude Longitude Altitude True airspeed Groundspeed vector Vertical velocity Attitude (pitch, roll, heading) relative flow angle (attack/sideslip)"
            },
            "relatedTo": {
                "ob_id": 24803,
                "uuid": "dea632c433ec4782a2e884e532bb22ee",
                "short_code": "acq",
                "title": "FAAM Flight C013 Acquisition",
                "abstract": "FAAM Flight C013 Acquisition"
            }
        },
        {
            "ob_id": 11293,
            "platform": {
                "ob_id": 24911,
                "uuid": "aa88bac8cf784828be77bffafe296474",
                "short_code": "plat",
                "title": "Charo (Mixed Palm Swamp)",
                "abstract": "An area of publicly owned land (Peru) used during field campaigns for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nThere are no formal arrangements for research in this area. MINAG and the Ministerio de Turismo in Iquitos need to be contacted to obtain research permits.\r\n\r\nLocation: 4°16'21.80\"S , 73°15'27.80\"W"
            },
            "instrument": {
                "ob_id": 19611,
                "uuid": "2bd5405d4aeb447eb5d41edd08ed7389",
                "short_code": "instr",
                "title": "University of St Andrews: Thermo TRACE Gas Chromatograph Ultra",
                "abstract": "The instrument is a gas chromatograph which is equipped with two FIDs (flame ionization detector) for carbon dioxide and methane. It also inclues an ECD (electron capture detector) for nitrous oxide. These are used for analysis of discrete air samples either injected by manual injection or via an auto-sampler. \r\n\r\nThe Thermo TRACE Gas Chromatograph Ultra (Thermo Fisher Scientific Inc. USA) instrument is hosted at the Department of Earth & Environmental Sciences, University of St Andrews. \r\n\r\nThis instrument measures concentrations of carbon dioxide, methane and nitrous oxide in discrete air samples.\r\n\r\nParameters listed in associated data files include: net_carbon_dioxide_flux, net_methane_flux, net_nitrous_oxide_flux"
            },
            "relatedTo": {
                "ob_id": 24912,
                "uuid": "3aaf817078724bc284b63d8505fe5a98",
                "short_code": "acq",
                "title": "Acquisition for Soil-atmosphere flux measurements calculated from concentration of methane and nitrous oxide taken from the Pastaza-Marañón foreland basin, Peru",
                "abstract": "6 campaign locations for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nAll samples were analysed back in the UK on the University of St Andrews Thermo TRACE Gas Chromatograph Ultra instrument. "
            }
        },
        {
            "ob_id": 11294,
            "platform": {
                "ob_id": 24910,
                "uuid": "86f8e34cc8c54d698ecb4d9e1af826ac",
                "short_code": "plat",
                "title": "San Jorge (M. flexuosa Palm Swamp)",
                "abstract": "An area of publicly owned land (Peru) used during field campaigns for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nThere are no formal arrangements for research in this area. MINAG and the Ministerio de Turismo in Iquitos need to be contacted to obtain research permits.\r\n\r\nLocation: 4°03'18.83\"S, 73°10'16.80\"W"
            },
            "instrument": {
                "ob_id": 19611,
                "uuid": "2bd5405d4aeb447eb5d41edd08ed7389",
                "short_code": "instr",
                "title": "University of St Andrews: Thermo TRACE Gas Chromatograph Ultra",
                "abstract": "The instrument is a gas chromatograph which is equipped with two FIDs (flame ionization detector) for carbon dioxide and methane. It also inclues an ECD (electron capture detector) for nitrous oxide. These are used for analysis of discrete air samples either injected by manual injection or via an auto-sampler. \r\n\r\nThe Thermo TRACE Gas Chromatograph Ultra (Thermo Fisher Scientific Inc. USA) instrument is hosted at the Department of Earth & Environmental Sciences, University of St Andrews. \r\n\r\nThis instrument measures concentrations of carbon dioxide, methane and nitrous oxide in discrete air samples.\r\n\r\nParameters listed in associated data files include: net_carbon_dioxide_flux, net_methane_flux, net_nitrous_oxide_flux"
            },
            "relatedTo": {
                "ob_id": 24912,
                "uuid": "3aaf817078724bc284b63d8505fe5a98",
                "short_code": "acq",
                "title": "Acquisition for Soil-atmosphere flux measurements calculated from concentration of methane and nitrous oxide taken from the Pastaza-Marañón foreland basin, Peru",
                "abstract": "6 campaign locations for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nAll samples were analysed back in the UK on the University of St Andrews Thermo TRACE Gas Chromatograph Ultra instrument. "
            }
        },
        {
            "ob_id": 11295,
            "platform": {
                "ob_id": 24909,
                "uuid": "ecb015d1673749e3a0dbf3499258dd0f",
                "short_code": "plat",
                "title": "Quistococha (M. flexuosa Palm Swamp)",
                "abstract": "An area of publicly owned land (Peru) used during field campaigns for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nThere are no formal arrangements for research in this area. MINAG and the Ministerio de Turismo in Iquitos need to be contacted to obtain research permits.\r\n\r\nLocation: 3°49'57.61\"S, 73°12'01.13\"W"
            },
            "instrument": {
                "ob_id": 19611,
                "uuid": "2bd5405d4aeb447eb5d41edd08ed7389",
                "short_code": "instr",
                "title": "University of St Andrews: Thermo TRACE Gas Chromatograph Ultra",
                "abstract": "The instrument is a gas chromatograph which is equipped with two FIDs (flame ionization detector) for carbon dioxide and methane. It also inclues an ECD (electron capture detector) for nitrous oxide. These are used for analysis of discrete air samples either injected by manual injection or via an auto-sampler. \r\n\r\nThe Thermo TRACE Gas Chromatograph Ultra (Thermo Fisher Scientific Inc. USA) instrument is hosted at the Department of Earth & Environmental Sciences, University of St Andrews. \r\n\r\nThis instrument measures concentrations of carbon dioxide, methane and nitrous oxide in discrete air samples.\r\n\r\nParameters listed in associated data files include: net_carbon_dioxide_flux, net_methane_flux, net_nitrous_oxide_flux"
            },
            "relatedTo": {
                "ob_id": 24912,
                "uuid": "3aaf817078724bc284b63d8505fe5a98",
                "short_code": "acq",
                "title": "Acquisition for Soil-atmosphere flux measurements calculated from concentration of methane and nitrous oxide taken from the Pastaza-Marañón foreland basin, Peru",
                "abstract": "6 campaign locations for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nAll samples were analysed back in the UK on the University of St Andrews Thermo TRACE Gas Chromatograph Ultra instrument. "
            }
        },
        {
            "ob_id": 11296,
            "platform": {
                "ob_id": 24908,
                "uuid": "6f358464ffcd4b7fbd16dfcc0bd979bb",
                "short_code": "plat",
                "title": "Miraflores (Forested Short Pole Vegetation)",
                "abstract": "An area of publicly owned land (Peru) used during field campaigns for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nThere are no formal arrangements for research in this area. MINAG and the Ministerio de Turismo in Iquitos need to be contacted to obtain research permits.\r\n\r\nLocation: 4°28'16.59\"S, 74° 4'39.95\"W"
            },
            "instrument": {
                "ob_id": 19611,
                "uuid": "2bd5405d4aeb447eb5d41edd08ed7389",
                "short_code": "instr",
                "title": "University of St Andrews: Thermo TRACE Gas Chromatograph Ultra",
                "abstract": "The instrument is a gas chromatograph which is equipped with two FIDs (flame ionization detector) for carbon dioxide and methane. It also inclues an ECD (electron capture detector) for nitrous oxide. These are used for analysis of discrete air samples either injected by manual injection or via an auto-sampler. \r\n\r\nThe Thermo TRACE Gas Chromatograph Ultra (Thermo Fisher Scientific Inc. USA) instrument is hosted at the Department of Earth & Environmental Sciences, University of St Andrews. \r\n\r\nThis instrument measures concentrations of carbon dioxide, methane and nitrous oxide in discrete air samples.\r\n\r\nParameters listed in associated data files include: net_carbon_dioxide_flux, net_methane_flux, net_nitrous_oxide_flux"
            },
            "relatedTo": {
                "ob_id": 24912,
                "uuid": "3aaf817078724bc284b63d8505fe5a98",
                "short_code": "acq",
                "title": "Acquisition for Soil-atmosphere flux measurements calculated from concentration of methane and nitrous oxide taken from the Pastaza-Marañón foreland basin, Peru",
                "abstract": "6 campaign locations for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nAll samples were analysed back in the UK on the University of St Andrews Thermo TRACE Gas Chromatograph Ultra instrument. "
            }
        },
        {
            "ob_id": 11297,
            "platform": {
                "ob_id": 24907,
                "uuid": "6910b16951554523b9708ab231edfae6",
                "short_code": "plat",
                "title": "San Jorge (Forested Short Pole Vegetation)",
                "abstract": "An area of publicly owned land (Peru) used during field campaigns for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nThere are no formal arrangements for research in this area. MINAG and the Ministerio de Turismo in Iquitos need to be contacted to obtain research permits.\r\n\r\nLocation: 4°03'35.95\"S, 73°12'01.13\"W"
            },
            "instrument": {
                "ob_id": 19611,
                "uuid": "2bd5405d4aeb447eb5d41edd08ed7389",
                "short_code": "instr",
                "title": "University of St Andrews: Thermo TRACE Gas Chromatograph Ultra",
                "abstract": "The instrument is a gas chromatograph which is equipped with two FIDs (flame ionization detector) for carbon dioxide and methane. It also inclues an ECD (electron capture detector) for nitrous oxide. These are used for analysis of discrete air samples either injected by manual injection or via an auto-sampler. \r\n\r\nThe Thermo TRACE Gas Chromatograph Ultra (Thermo Fisher Scientific Inc. USA) instrument is hosted at the Department of Earth & Environmental Sciences, University of St Andrews. \r\n\r\nThis instrument measures concentrations of carbon dioxide, methane and nitrous oxide in discrete air samples.\r\n\r\nParameters listed in associated data files include: net_carbon_dioxide_flux, net_methane_flux, net_nitrous_oxide_flux"
            },
            "relatedTo": {
                "ob_id": 24912,
                "uuid": "3aaf817078724bc284b63d8505fe5a98",
                "short_code": "acq",
                "title": "Acquisition for Soil-atmosphere flux measurements calculated from concentration of methane and nitrous oxide taken from the Pastaza-Marañón foreland basin, Peru",
                "abstract": "6 campaign locations for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nAll samples were analysed back in the UK on the University of St Andrews Thermo TRACE Gas Chromatograph Ultra instrument. "
            }
        },
        {
            "ob_id": 11298,
            "platform": {
                "ob_id": 24906,
                "uuid": "9c32d97ec6294da495d44dbfe7821bd6",
                "short_code": "plat",
                "title": "Buena Vista (Forested Vegetation)",
                "abstract": "An area of publicly owned land (Peru) used during field campaigns for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nThere are no formal arrangements for research in this area. MINAG and the Ministerio de Turismo in Iquitos need to be contacted to obtain research permits.\r\n\r\nLocation: 4°14'45.60\"S, 73°12'0.20\"W"
            },
            "instrument": {
                "ob_id": 19611,
                "uuid": "2bd5405d4aeb447eb5d41edd08ed7389",
                "short_code": "instr",
                "title": "University of St Andrews: Thermo TRACE Gas Chromatograph Ultra",
                "abstract": "The instrument is a gas chromatograph which is equipped with two FIDs (flame ionization detector) for carbon dioxide and methane. It also inclues an ECD (electron capture detector) for nitrous oxide. These are used for analysis of discrete air samples either injected by manual injection or via an auto-sampler. \r\n\r\nThe Thermo TRACE Gas Chromatograph Ultra (Thermo Fisher Scientific Inc. USA) instrument is hosted at the Department of Earth & Environmental Sciences, University of St Andrews. \r\n\r\nThis instrument measures concentrations of carbon dioxide, methane and nitrous oxide in discrete air samples.\r\n\r\nParameters listed in associated data files include: net_carbon_dioxide_flux, net_methane_flux, net_nitrous_oxide_flux"
            },
            "relatedTo": {
                "ob_id": 24912,
                "uuid": "3aaf817078724bc284b63d8505fe5a98",
                "short_code": "acq",
                "title": "Acquisition for Soil-atmosphere flux measurements calculated from concentration of methane and nitrous oxide taken from the Pastaza-Marañón foreland basin, Peru",
                "abstract": "6 campaign locations for the NERC project: Amazonian peatlands - A potentially important but poorly characterised source of atmospheric methane and nitrous oxide (NE/I015469/2).\r\n\r\nAll samples were analysed back in the UK on the University of St Andrews Thermo TRACE Gas Chromatograph Ultra instrument. "
            }
        },
        {
            "ob_id": 11299,
            "platform": {
                "ob_id": 1416,
                "uuid": "1c1c59696701483d90ea04c428c67c09",
                "short_code": "plat",
                "title": "NCAS Weybourne Atmospheric Observatory",
                "abstract": "The National Centre for Atmospheric Science's Weybourne Atmospheric Observatory (WAO) is a Regional station in the Global Atmosphere Watch (GAW) programme of the World Meteorological Organization (WMO). It is situated on the North Norfolk coast (52°57’02’’N, 1°07’19’’E, 15 m asl). Weybourne is operated by the  School of Environmental Sciences at the University of East Anglia (UEA) having been established in 1992 by Professor Stuart Penkett (retired 2004) with funding from BP (Norway) plc and NERC.  Subsequently, long term monitoring and campaigns have been supported through numerous projects funded by NERC, Department of the Environment (DoE, Defra) and the EU.  NCAS has also supported the site since 2002. Much of the instrumentation has come from HEFCE JIF and SRIF funds.\r\n\r\nWeybourne’s location means that it experiences air with a wide range of pollution levels.  Predominant south-westerlies bring polluted air from the UK (including from London and the Midlands).  At times, especially in anticyclonic conditions, Weybourne experiences polluted air from Europe.  Weybourne can also receive clean background air in northerly air flow.  This can be impacted by narrow pollution plumes from shipping in the N. Sea, and potentially gas platforms. Many successful campaigns have been hosted at Weybourne to examine oxidizing capacity, organic chemistry, carbonaceous particles, night-time chemistry and cloud impacts on radiation.  In addition to the permanent building (see photo) there is adequate power and space to support instrumented mobile labs and containers.  The site is also used by the wider community for instrument testing."
            },
            "instrument": {
                "ob_id": 15415,
                "uuid": "02b5230cf5e8409abac700eee58dda79",
                "short_code": "instr",
                "title": "New Instrument: man-cims",
                "abstract": "New instrument created, more details to follow for instrument man-cims"
            },
            "relatedTo": {
                "ob_id": 24948,
                "uuid": "0f8731f7a2294f19a145bfcad233def0",
                "short_code": "acq",
                "title": "Measurements of N2O5, ClNO2, HCOOH, HNO3 and HCN at the Weybourne Atmospheric Observatory",
                "abstract": "Measurements of N2O5, ClNO2, HCOOH, HNO3 and HCN at the Weybourne Atmospheric Observatory"
            }
        },
        {
            "ob_id": 11300,
            "platform": {
                "ob_id": 24964,
                "uuid": "97ada28c616a41f18be7e5ccd1a90837",
                "short_code": "plat",
                "title": "Met Éireann Knock Airport meteorological station",
                "abstract": "Ireland West Airport Knock (IATA: NOC, ICAO: EIKN) (Irish: Aerfort Iarthar Éireann Chnoc Mhuire) is an airport 5.6 km (3.5 miles) south-west of Charlestown, County Mayo, north-west Ireland. The village of Knock is 20 km (12.5 miles) away and is the fourth busiest in the Republic of Ireland after Dublin, Cork and Shannon.\r\n\r\nThe meteorological station at the site operates a variety of instruments including a ceilometer and has a WMO ID 03973.\r\n\r\nThe site is located 203m elevation about mean sea level."
            },
            "instrument": {
                "ob_id": 12455,
                "uuid": "51aeccff6bdb45bdaa0a4b33a7b49cdb",
                "short_code": "instr",
                "title": "Met Éireann: Vaisala CL31 Ceilometer",
                "abstract": "The Met Éireann own a number of Vaisala CL31 ceilometers used for detecting cloud base heights and also for obtaining backscatter profiles to aid ash cloud detection.  The CL31 employs a pulsed diode laser LIDAR (light detection and ranging) technology, which enables it to detect three cloud layers simultaneously.\r\n\r\nFast measurement helps to detect thin cloud patches below a solid cloud base. The CL31 provides a full backscatter profile for data visualization and research purpose. The CL31 beam can be directed either vertically or tilted. The tilting option together with the novel optics design provides enhanced performance during precipitation by improving the protection given by the shield. In the measurement unit, a tilt angle sensor automatically corrects the measured cloud distance reading to vertical cloud base height."
            },
            "relatedTo": {
                "ob_id": 24963,
                "uuid": "2e54960007734be4a8e5a8780a44ea4f",
                "short_code": "acq",
                "title": "Vaisala Cl31 Ceilometer at Knock Airport",
                "abstract": "Vaisala Cl31 Ceilometer deployed at Knock Airport as part of the Met Éireann's LIDARNET network."
            }
        },
        {
            "ob_id": 11301,
            "platform": {
                "ob_id": 24868,
                "uuid": "210c62de726d4880a094ce01ab74ae59",
                "short_code": "plat",
                "title": "Amazonica private rented aircraft",
                "abstract": "The Amazonica aircraft is a private aircraft used for taking air samples above ground sites during the Amazonica project. Air is sucked via an inlet outside the aircraft into unit filled with flasks. These flasks are subsequently shipped to and analyzed at high-precision gas analytics laboratory at INPE, Sao Jose dos Campos, Brazil."
            },
            "instrument": {
                "ob_id": 25434,
                "uuid": "692fc5e7632a44d4b816f856a2af83a2",
                "short_code": "instr",
                "title": "Amazonica: FID (Flame Ionization Detector) chromatography",
                "abstract": "Methane measurements were collected for the Amazonica project using a FID (Flame Ionization Detector) chromatography (HP 6890 Plus) with a 198 cm, 3/16″ O.D. precolumn of length (Silica Gel 80/100mesh) \r\nand a 106 cm ~ 3/16″ O.D. analytical column (Molecular Sieve 5A 80/100mesh) and a 12 mL sample loop.\r\n"
            },
            "relatedTo": {
                "ob_id": 24971,
                "uuid": "33c3a3dd82374668bdb23331fc52e2b1",
                "short_code": "acq",
                "title": "Amazonica",
                "abstract": "Amazonica"
            }
        },
        {
            "ob_id": 11302,
            "platform": {
                "ob_id": 24867,
                "uuid": "672ad3457117471ebd7d2f4e15f1504d",
                "short_code": "plat",
                "title": "Institute of Atmospheric Physics land station, Beijing",
                "abstract": "The Institute of Atmospheric Physics in Bejing is a ground measurement site for the Atmospheric Pollution & Human Health in a Chinese Megacity programme (APHH-Beijing) intensive field campaigns."
            },
            "instrument": {
                "ob_id": 13069,
                "uuid": "3f21274cd3ba40d391b154f87bfc9f25",
                "short_code": "instr",
                "title": "University of York's TEI 49 UV absorption O3 analyser",
                "abstract": "The Thermo 49 is a powerful, easy-to-use, UV photometric based ozone analyzer which offers increased specificity via its balanced optical system. User programmable software capabilities allows selection of the frequency at which internalzero/span activation and instrument calibrationchecks will occur. Additionally, field programmable measurement range settings can bestored in memory for subsequent recall. Extended troubleshooting diagnostics now provide instantaneous indication of instrumentoperating parameter, status including: Pressure, Flow, DC Supply Voltages, Optical BenchTemperature, Ozonator Power Supply Voltageand Lamp Voltage.\r\n\r\nThermo Environmental Instruments 49i UV absorption O3 analyser under AMF and currently operated by the University of Leeds. This is a ground-based laser-induced fluorescence instrument for detection of OH, HO2, and RO2 radicals. OH reactivity measurements using a laser flash-photolysis technique can be provided alongside the radical measurements. The instrument is housed in and operated from a custom-built 20 ft shipping container."
            },
            "relatedTo": {
                "ob_id": 24980,
                "uuid": "493ff805be3546f990ed326ea1a44233",
                "short_code": "acq",
                "title": "APHH: O3, CO, NO, NO2, NOy and SO2 measurements made at the IAP-Beijing site during the summer and winter",
                "abstract": "APHH: O3, CO, NO, NO2, NOy and SO2 measurements made at the IAP-Beijing site during the summer"
            }
        },
        {
            "ob_id": 11304,
            "platform": {
                "ob_id": 24867,
                "uuid": "672ad3457117471ebd7d2f4e15f1504d",
                "short_code": "plat",
                "title": "Institute of Atmospheric Physics land station, Beijing",
                "abstract": "The Institute of Atmospheric Physics in Bejing is a ground measurement site for the Atmospheric Pollution & Human Health in a Chinese Megacity programme (APHH-Beijing) intensive field campaigns."
            },
            "instrument": {
                "ob_id": 24976,
                "uuid": "f3a3a1404ca64118ae8a498a002f4d85",
                "short_code": "instr",
                "title": "University of York: TEI 42i TL NO analyser",
                "abstract": "NO data taken using a TEI 42i TL NO analyser. NO instrument calibrated using 100ppb NO in nitrogen cylinder (BOC - certified to NPL standard)\r\n\r\n"
            },
            "relatedTo": {
                "ob_id": 24980,
                "uuid": "493ff805be3546f990ed326ea1a44233",
                "short_code": "acq",
                "title": "APHH: O3, CO, NO, NO2, NOy and SO2 measurements made at the IAP-Beijing site during the summer and winter",
                "abstract": "APHH: O3, CO, NO, NO2, NOy and SO2 measurements made at the IAP-Beijing site during the summer"
            }
        },
        {
            "ob_id": 11305,
            "platform": {
                "ob_id": 24867,
                "uuid": "672ad3457117471ebd7d2f4e15f1504d",
                "short_code": "plat",
                "title": "Institute of Atmospheric Physics land station, Beijing",
                "abstract": "The Institute of Atmospheric Physics in Bejing is a ground measurement site for the Atmospheric Pollution & Human Health in a Chinese Megacity programme (APHH-Beijing) intensive field campaigns."
            },
            "instrument": {
                "ob_id": 24977,
                "uuid": "eb912f987efd4df4bc30d0520dbad063",
                "short_code": "instr",
                "title": "University of York: Teledyne T500~U CAPS analyser",
                "abstract": "NO2 data taken using Teledyne T500~U CAPS analyser. NO2 instrument calibrated using 100ppb NO2 in nitrogen cylinder (BOC)\r\n"
            },
            "relatedTo": {
                "ob_id": 24980,
                "uuid": "493ff805be3546f990ed326ea1a44233",
                "short_code": "acq",
                "title": "APHH: O3, CO, NO, NO2, NOy and SO2 measurements made at the IAP-Beijing site during the summer and winter",
                "abstract": "APHH: O3, CO, NO, NO2, NOy and SO2 measurements made at the IAP-Beijing site during the summer"
            }
        }
    ]
}