Instrument Platform Pair List

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    "count": 14115,
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    "results": [
        {
            "ob_id": 12231,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 7946,
                "uuid": "085948b19c544a5683b548a80834d3ec",
                "short_code": "instr",
                "title": "ARSF Specim AISA Eagle",
                "abstract": "The AISA Eagle is a 12 bit, pushbroom, hyperspectral sensor with a 1000 pixel swath width, covering the visible and near infra-red spectrum 400 - 970nm. The maximum spectral resolution of the sensor is 2.9nm. Also output to the Eagle are data from the fibre optic downwelling irradiance sensor (FODIS). \r\n\r\nThe AISA Eagle requires good atmospheric conditions for the collection of narrow spectral wavebands. In the UK we are yet to collect data better that 2.5nm bandwidth (spectrally binning by 2). In less than perfect illumination or atmospheric conditions the instrument may require spectral and/or spatial binning to allow data to be collected. Should perfect optical conditions be essential for your project then there can be no guarantee that these conditions may coincide with the availability of the aircraft in a single flying season. If this project depends on its support in the flying season immediately following the year of submission (or if spectral quality is less of a concern) then additional guidance concerning spatial and spectral binning should be sought."
            },
            "relatedTo": null
        },
        {
            "ob_id": 12232,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 10567,
                "uuid": "b0b464be7fef4f9fb8d568443097b9cb",
                "short_code": "instr",
                "title": "ARSF Specim AISA Hawk",
                "abstract": "The AISA Hawk is a 14 bit sensor able to capture short wave infrared wavelengths, 970 - 2450nm. This makes the Hawk an ideal tool for data acquisition on spectral signatures characteristic to chemical compounds and man-made targets that can not be distinguished using the Eagle instrument. The Hawk has 320 spatial pixels, 244 spectral pixels and a maximum spectral resolution of 8nm."
            },
            "relatedTo": null
        },
        {
            "ob_id": 12233,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 10567,
                "uuid": "b0b464be7fef4f9fb8d568443097b9cb",
                "short_code": "instr",
                "title": "ARSF Specim AISA Hawk",
                "abstract": "The AISA Hawk is a 14 bit sensor able to capture short wave infrared wavelengths, 970 - 2450nm. This makes the Hawk an ideal tool for data acquisition on spectral signatures characteristic to chemical compounds and man-made targets that can not be distinguished using the Eagle instrument. The Hawk has 320 spatial pixels, 244 spectral pixels and a maximum spectral resolution of 8nm."
            },
            "relatedTo": null
        },
        {
            "ob_id": 12234,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 7946,
                "uuid": "085948b19c544a5683b548a80834d3ec",
                "short_code": "instr",
                "title": "ARSF Specim AISA Eagle",
                "abstract": "The AISA Eagle is a 12 bit, pushbroom, hyperspectral sensor with a 1000 pixel swath width, covering the visible and near infra-red spectrum 400 - 970nm. The maximum spectral resolution of the sensor is 2.9nm. Also output to the Eagle are data from the fibre optic downwelling irradiance sensor (FODIS). \r\n\r\nThe AISA Eagle requires good atmospheric conditions for the collection of narrow spectral wavebands. In the UK we are yet to collect data better that 2.5nm bandwidth (spectrally binning by 2). In less than perfect illumination or atmospheric conditions the instrument may require spectral and/or spatial binning to allow data to be collected. Should perfect optical conditions be essential for your project then there can be no guarantee that these conditions may coincide with the availability of the aircraft in a single flying season. If this project depends on its support in the flying season immediately following the year of submission (or if spectral quality is less of a concern) then additional guidance concerning spatial and spectral binning should be sought."
            },
            "relatedTo": null
        },
        {
            "ob_id": 12235,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": null
        },
        {
            "ob_id": 12236,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": null
        },
        {
            "ob_id": 12237,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": null
        },
        {
            "ob_id": 12238,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": null
        },
        {
            "ob_id": 12239,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 7946,
                "uuid": "085948b19c544a5683b548a80834d3ec",
                "short_code": "instr",
                "title": "ARSF Specim AISA Eagle",
                "abstract": "The AISA Eagle is a 12 bit, pushbroom, hyperspectral sensor with a 1000 pixel swath width, covering the visible and near infra-red spectrum 400 - 970nm. The maximum spectral resolution of the sensor is 2.9nm. Also output to the Eagle are data from the fibre optic downwelling irradiance sensor (FODIS). \r\n\r\nThe AISA Eagle requires good atmospheric conditions for the collection of narrow spectral wavebands. In the UK we are yet to collect data better that 2.5nm bandwidth (spectrally binning by 2). In less than perfect illumination or atmospheric conditions the instrument may require spectral and/or spatial binning to allow data to be collected. Should perfect optical conditions be essential for your project then there can be no guarantee that these conditions may coincide with the availability of the aircraft in a single flying season. If this project depends on its support in the flying season immediately following the year of submission (or if spectral quality is less of a concern) then additional guidance concerning spatial and spectral binning should be sought."
            },
            "relatedTo": null
        },
        {
            "ob_id": 12240,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 10567,
                "uuid": "b0b464be7fef4f9fb8d568443097b9cb",
                "short_code": "instr",
                "title": "ARSF Specim AISA Hawk",
                "abstract": "The AISA Hawk is a 14 bit sensor able to capture short wave infrared wavelengths, 970 - 2450nm. This makes the Hawk an ideal tool for data acquisition on spectral signatures characteristic to chemical compounds and man-made targets that can not be distinguished using the Eagle instrument. The Hawk has 320 spatial pixels, 244 spectral pixels and a maximum spectral resolution of 8nm."
            },
            "relatedTo": null
        },
        {
            "ob_id": 12241,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 28068,
                "uuid": "90c5bbbc85f64fc484d02032dcf5fcff",
                "short_code": "acq",
                "title": "ARSF 2013_222a - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_222a - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12242,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 28068,
                "uuid": "90c5bbbc85f64fc484d02032dcf5fcff",
                "short_code": "acq",
                "title": "ARSF 2013_222a - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_222a - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12243,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 7946,
                "uuid": "085948b19c544a5683b548a80834d3ec",
                "short_code": "instr",
                "title": "ARSF Specim AISA Eagle",
                "abstract": "The AISA Eagle is a 12 bit, pushbroom, hyperspectral sensor with a 1000 pixel swath width, covering the visible and near infra-red spectrum 400 - 970nm. The maximum spectral resolution of the sensor is 2.9nm. Also output to the Eagle are data from the fibre optic downwelling irradiance sensor (FODIS). \r\n\r\nThe AISA Eagle requires good atmospheric conditions for the collection of narrow spectral wavebands. In the UK we are yet to collect data better that 2.5nm bandwidth (spectrally binning by 2). In less than perfect illumination or atmospheric conditions the instrument may require spectral and/or spatial binning to allow data to be collected. Should perfect optical conditions be essential for your project then there can be no guarantee that these conditions may coincide with the availability of the aircraft in a single flying season. If this project depends on its support in the flying season immediately following the year of submission (or if spectral quality is less of a concern) then additional guidance concerning spatial and spectral binning should be sought."
            },
            "relatedTo": {
                "ob_id": 28068,
                "uuid": "90c5bbbc85f64fc484d02032dcf5fcff",
                "short_code": "acq",
                "title": "ARSF 2013_222a - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_222a - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12244,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 10567,
                "uuid": "b0b464be7fef4f9fb8d568443097b9cb",
                "short_code": "instr",
                "title": "ARSF Specim AISA Hawk",
                "abstract": "The AISA Hawk is a 14 bit sensor able to capture short wave infrared wavelengths, 970 - 2450nm. This makes the Hawk an ideal tool for data acquisition on spectral signatures characteristic to chemical compounds and man-made targets that can not be distinguished using the Eagle instrument. The Hawk has 320 spatial pixels, 244 spectral pixels and a maximum spectral resolution of 8nm."
            },
            "relatedTo": {
                "ob_id": 28068,
                "uuid": "90c5bbbc85f64fc484d02032dcf5fcff",
                "short_code": "acq",
                "title": "ARSF 2013_222a - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_222a - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12245,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 10567,
                "uuid": "b0b464be7fef4f9fb8d568443097b9cb",
                "short_code": "instr",
                "title": "ARSF Specim AISA Hawk",
                "abstract": "The AISA Hawk is a 14 bit sensor able to capture short wave infrared wavelengths, 970 - 2450nm. This makes the Hawk an ideal tool for data acquisition on spectral signatures characteristic to chemical compounds and man-made targets that can not be distinguished using the Eagle instrument. The Hawk has 320 spatial pixels, 244 spectral pixels and a maximum spectral resolution of 8nm."
            },
            "relatedTo": {
                "ob_id": 28069,
                "uuid": "4daa6961be764f99b9d8525364c2721b",
                "short_code": "acq",
                "title": "ARSF 2013_222b - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_222b - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12246,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 7946,
                "uuid": "085948b19c544a5683b548a80834d3ec",
                "short_code": "instr",
                "title": "ARSF Specim AISA Eagle",
                "abstract": "The AISA Eagle is a 12 bit, pushbroom, hyperspectral sensor with a 1000 pixel swath width, covering the visible and near infra-red spectrum 400 - 970nm. The maximum spectral resolution of the sensor is 2.9nm. Also output to the Eagle are data from the fibre optic downwelling irradiance sensor (FODIS). \r\n\r\nThe AISA Eagle requires good atmospheric conditions for the collection of narrow spectral wavebands. In the UK we are yet to collect data better that 2.5nm bandwidth (spectrally binning by 2). In less than perfect illumination or atmospheric conditions the instrument may require spectral and/or spatial binning to allow data to be collected. Should perfect optical conditions be essential for your project then there can be no guarantee that these conditions may coincide with the availability of the aircraft in a single flying season. If this project depends on its support in the flying season immediately following the year of submission (or if spectral quality is less of a concern) then additional guidance concerning spatial and spectral binning should be sought."
            },
            "relatedTo": {
                "ob_id": 28069,
                "uuid": "4daa6961be764f99b9d8525364c2721b",
                "short_code": "acq",
                "title": "ARSF 2013_222b - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_222b - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12247,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 28069,
                "uuid": "4daa6961be764f99b9d8525364c2721b",
                "short_code": "acq",
                "title": "ARSF 2013_222b - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_222b - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12248,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 28069,
                "uuid": "4daa6961be764f99b9d8525364c2721b",
                "short_code": "acq",
                "title": "ARSF 2013_222b - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_222b - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12249,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 28070,
                "uuid": "609c6adde5f5413cbc57d51dbc7dabc2",
                "short_code": "acq",
                "title": "ARSF 2013_223 - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_223 - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12250,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 28070,
                "uuid": "609c6adde5f5413cbc57d51dbc7dabc2",
                "short_code": "acq",
                "title": "ARSF 2013_223 - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_223 - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12251,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 7946,
                "uuid": "085948b19c544a5683b548a80834d3ec",
                "short_code": "instr",
                "title": "ARSF Specim AISA Eagle",
                "abstract": "The AISA Eagle is a 12 bit, pushbroom, hyperspectral sensor with a 1000 pixel swath width, covering the visible and near infra-red spectrum 400 - 970nm. The maximum spectral resolution of the sensor is 2.9nm. Also output to the Eagle are data from the fibre optic downwelling irradiance sensor (FODIS). \r\n\r\nThe AISA Eagle requires good atmospheric conditions for the collection of narrow spectral wavebands. In the UK we are yet to collect data better that 2.5nm bandwidth (spectrally binning by 2). In less than perfect illumination or atmospheric conditions the instrument may require spectral and/or spatial binning to allow data to be collected. Should perfect optical conditions be essential for your project then there can be no guarantee that these conditions may coincide with the availability of the aircraft in a single flying season. If this project depends on its support in the flying season immediately following the year of submission (or if spectral quality is less of a concern) then additional guidance concerning spatial and spectral binning should be sought."
            },
            "relatedTo": {
                "ob_id": 28070,
                "uuid": "609c6adde5f5413cbc57d51dbc7dabc2",
                "short_code": "acq",
                "title": "ARSF 2013_223 - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_223 - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12252,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 10567,
                "uuid": "b0b464be7fef4f9fb8d568443097b9cb",
                "short_code": "instr",
                "title": "ARSF Specim AISA Hawk",
                "abstract": "The AISA Hawk is a 14 bit sensor able to capture short wave infrared wavelengths, 970 - 2450nm. This makes the Hawk an ideal tool for data acquisition on spectral signatures characteristic to chemical compounds and man-made targets that can not be distinguished using the Eagle instrument. The Hawk has 320 spatial pixels, 244 spectral pixels and a maximum spectral resolution of 8nm."
            },
            "relatedTo": {
                "ob_id": 28070,
                "uuid": "609c6adde5f5413cbc57d51dbc7dabc2",
                "short_code": "acq",
                "title": "ARSF 2013_223 - IG13_21 Flight: data acquisition details",
                "abstract": "ARSF 2013_223 - IG13_21 Flight: data acquisition details."
            }
        },
        {
            "ob_id": 12261,
            "platform": {
                "ob_id": 8207,
                "uuid": "3f2dbe69fe4c40ee9e1e8be87e15a1d5",
                "short_code": "plat",
                "title": "Metop-A",
                "abstract": "Metop-A, launched on 19 October 2006, represents the first in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS). Metop-A is Europe's first polar-orbiting meteorological satellite"
            },
            "instrument": {
                "ob_id": 8451,
                "uuid": "a78c6eb7196f42c7a482317ebe638758",
                "short_code": "instr",
                "title": "AVHRR series",
                "abstract": "The Advanced Very High Resolution Radiometer (AVHRR) sensor is a broad-band, 4- or 5- channel scanning radiometer, sensing in the visible, near-infrared, and thermal infrared. Its objective is to provide radiance data for investigation of clouds, land-water boundaries, snow and ice extent, ice or snow melt inception, day and night cloud distribution, temperatures of radiating surfaces, and sea surface temperature. Other applications include agricultural assessment, land cover mapping, production of large-area maps, and evaluation of regional and continental snow cover."
            },
            "relatedTo": {
                "ob_id": 28091,
                "uuid": "44678a0f3db246c9afd4d3c92d3659c3",
                "short_code": "acq",
                "title": "FIDUCEO V1.0 AVHRR Ensemble FCDR data acquisition",
                "abstract": "FIDUCEO V1.0 AVHRR FCDR data acquisition from NOAA and Metop A satellites"
            }
        },
        {
            "ob_id": 12262,
            "platform": {
                "ob_id": 28095,
                "uuid": "2d34269b1f1b45c785724a912989be90",
                "short_code": "plat",
                "title": "Chulabhorn Research Institute Building, Lak Si",
                "abstract": "Chulabhorn Research Institute is a biomedical and chemistry research institute in Bangkok, Thailand."
            },
            "instrument": {
                "ob_id": 28094,
                "uuid": "95119f0a3b1f4c0bb0846b3dd08055d0",
                "short_code": "instr",
                "title": "University of Bristol: Sven Leckel LVS3",
                "abstract": "Sven Leckel LVS3 is a particle sampler."
            },
            "relatedTo": {
                "ob_id": 28096,
                "uuid": "9133cf0d4a9f4d518941488443cd3cfe",
                "short_code": "acq",
                "title": "PM10 concentration and composition measurements in Lak Si, Bangkok, Thailand",
                "abstract": "PM10 concentration and composition measurements in Lak Si, Bangkok, Thailand"
            }
        },
        {
            "ob_id": 12263,
            "platform": {
                "ob_id": 28095,
                "uuid": "2d34269b1f1b45c785724a912989be90",
                "short_code": "plat",
                "title": "Chulabhorn Research Institute Building, Lak Si",
                "abstract": "Chulabhorn Research Institute is a biomedical and chemistry research institute in Bangkok, Thailand."
            },
            "instrument": {
                "ob_id": 28099,
                "uuid": "d5703a524ab7469fa17a07542efe93ff",
                "short_code": "instr",
                "title": "Gill Maximet 501 Weather station",
                "abstract": "Gill Maximet 501 Weather station"
            },
            "relatedTo": {
                "ob_id": 28096,
                "uuid": "9133cf0d4a9f4d518941488443cd3cfe",
                "short_code": "acq",
                "title": "PM10 concentration and composition measurements in Lak Si, Bangkok, Thailand",
                "abstract": "PM10 concentration and composition measurements in Lak Si, Bangkok, Thailand"
            }
        },
        {
            "ob_id": 12264,
            "platform": {
                "ob_id": 28095,
                "uuid": "2d34269b1f1b45c785724a912989be90",
                "short_code": "plat",
                "title": "Chulabhorn Research Institute Building, Lak Si",
                "abstract": "Chulabhorn Research Institute is a biomedical and chemistry research institute in Bangkok, Thailand."
            },
            "instrument": {
                "ob_id": 28100,
                "uuid": "7d68d7435d2e4f7393638863ce62b5e3",
                "short_code": "instr",
                "title": "Gill Maximet 100 weather station",
                "abstract": "Gill Maximet 100 weather station"
            },
            "relatedTo": {
                "ob_id": 28096,
                "uuid": "9133cf0d4a9f4d518941488443cd3cfe",
                "short_code": "acq",
                "title": "PM10 concentration and composition measurements in Lak Si, Bangkok, Thailand",
                "abstract": "PM10 concentration and composition measurements in Lak Si, Bangkok, Thailand"
            }
        },
        {
            "ob_id": 12265,
            "platform": {
                "ob_id": 1679,
                "uuid": "25e813e1539d46aeaf320dc3e4f06b8f",
                "short_code": "plat",
                "title": "NOAA-9",
                "abstract": "NASA polar-orbiting satellite which operated for the period december 1984 to August 1993."
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12266,
            "platform": {
                "ob_id": 1686,
                "uuid": "23ca6bfcca9342a18cc15e7b2f3e7e60",
                "short_code": "plat",
                "title": "NOAA-10",
                "abstract": "NASA polar-orbiting satellite which operated for the period September 1986 to September 1991."
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12267,
            "platform": {
                "ob_id": 1693,
                "uuid": "922c7e6cc7d04fa78ca9b30cd4d646c8",
                "short_code": "plat",
                "title": "NOAA-11",
                "abstract": "NASA polar orbiting satellite which operated during the period 24 Spetember 1988 to March 1995."
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12268,
            "platform": {
                "ob_id": 1801,
                "uuid": "899ad53a29ea4232888f2d021dd988d3",
                "short_code": "plat",
                "title": "NOAA-12",
                "abstract": "NASA polar orbiting satellite which was launched on May 14, 1991 remained operational until April 2001."
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12269,
            "platform": {
                "ob_id": 1809,
                "uuid": "e43da72c118e44ec811c395aa05a16be",
                "short_code": "plat",
                "title": "NOAA-14",
                "abstract": "NOAA polar orbiting satellite which operated during the period 30 December 1994 to Febraury 2001."
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12270,
            "platform": {
                "ob_id": 1816,
                "uuid": "a6fa2998eb0246b4a699a0753c74a2f3",
                "short_code": "plat",
                "title": "NOAA-15",
                "abstract": "NOAA polar orbiting satellite which was launched on May 13, 1998 and is still operational to this date."
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12271,
            "platform": {
                "ob_id": 1824,
                "uuid": "2a13c66bfad74b98b9cd4201c51de8c1",
                "short_code": "plat",
                "title": "NOAA-16",
                "abstract": "NOAA polar orbiting satellite which was launched on September 21, 2000"
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12272,
            "platform": {
                "ob_id": 1831,
                "uuid": "4e8478da0c034af08d057e85dd4536be",
                "short_code": "plat",
                "title": "NOAA-17",
                "abstract": "NOAA polar orbiting satellite which was launched on June 24, 2002."
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12273,
            "platform": {
                "ob_id": 27174,
                "uuid": "3dba7abe842a4f55b7d27d58cfa6b7ac",
                "short_code": "plat",
                "title": "NOAA-18",
                "abstract": "NOAA (National Oceanic and Atmospheric Administration) polar orbiting satellite which was launched on 20th May, 2005."
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12274,
            "platform": {
                "ob_id": 27175,
                "uuid": "c6470e63d7f84f20b9c765be3d0b9352",
                "short_code": "plat",
                "title": "NOAA-19",
                "abstract": "NOAA (National Oceanic and Atmospheric Administration) polar orbiting satellite which was launched on 6th February 2009"
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12275,
            "platform": {
                "ob_id": 8207,
                "uuid": "3f2dbe69fe4c40ee9e1e8be87e15a1d5",
                "short_code": "plat",
                "title": "Metop-A",
                "abstract": "Metop-A, launched on 19 October 2006, represents the first in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS). Metop-A is Europe's first polar-orbiting meteorological satellite"
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12276,
            "platform": {
                "ob_id": 8299,
                "uuid": "84a6355ac58249cc8c636e77a243c86a",
                "short_code": "plat",
                "title": "Metop-B",
                "abstract": "Metop-B, launched on the 17th September 2012, is the second in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS)."
            },
            "instrument": {
                "ob_id": 28103,
                "uuid": "5698692417e140a1a3d5e5564c43fafa",
                "short_code": "instr",
                "title": "High-resolution Infrared Radiation Sounder (HIRS)",
                "abstract": "HIRS is a 20-channel infrared scanning radiometer that performs operational atmospheric sounding.\r\n\r\nHIRS has 19 infrared channels (3.8-15 µm) and one visible channel. The swath width is 2160 km, with a 10 km resolution at nadir.\r\n\r\nIR calibration of the HIRS/4 is provided by programmed views of two radiometric targets mdash; the warm target, mounted on the instrument baseplate, and a view of deep space. Data from these views provides sensitivity calibrations for each channel at 256 second intervals, if commanded. Internally generated electronic signals provide calibration and stability monitoring of the detector amplifier and signal processing electronics.\r\n\r\nHIRS uses CO2 absorption bands for temperature sounding (CO2 is uniformly mixed in the atmosphere). HIRS also measures water vapour, ozone, N2O and cloud and surface temperatures."
            },
            "relatedTo": {
                "ob_id": 28102,
                "uuid": "1151de63ae1f447eb8ae449e9e137dfc",
                "short_code": "acq",
                "title": "FIDUCEO HIRS V1.0 data aquisition",
                "abstract": "FIDUCEO HIRS V1.0 data aquisition;  Core input data are L1B data files obtained from the NOAA CLASS archive. Spectral response functions are  obtained from NOAA NESDIS STAR PRT coefficients are obtained from CPIDS and also provided by NOAA"
            }
        },
        {
            "ob_id": 12277,
            "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": 28135,
                "uuid": "00a914c3108840debcf093fe14cbebe0",
                "short_code": "instr",
                "title": "Weybourne Atmospheric Observatory: NCAS Fourier Transform Infra-Red (FTIR)",
                "abstract": "Weybourne Atmospheric Observatory:  Fourier Transform Infra-Red (FTIR) measures CH4, N2O, CO and CO2. it is operated at WAO on behalf of National Centre for Atmospheric Science (NCAS). \r\nThe ECOTECH Spectronus™ is an FTIR spectrometer coupled to a multi-pass cell and a gas sampling manifold. It is principally intended for in situ sampling and analysis of air. The analyser is fully automated and provides real-time concentration or mole fraction measurements of target gases including N2O, CH4 , CO, CO2."
            },
            "relatedTo": {
                "ob_id": 28136,
                "uuid": "c4ed2ce13e8a40db8b48c7077019f7d9",
                "short_code": "acq",
                "title": "Weybourne Atmospheric Observatory: Fourier Transform Infra-Red (FTIR) measurements",
                "abstract": "Weybourne Atmospheric Observatory: Fourier Transform Infra-Red (FTIR) measurements"
            }
        },
        {
            "ob_id": 12278,
            "platform": {
                "ob_id": 28183,
                "uuid": "9f054fdc53d04b88a704cd9cf9f256cd",
                "short_code": "plat",
                "title": "Kjølnes Atmospheric Observatory (KJN)",
                "abstract": "Kjølnes Atmospheric Observatory (KJN) (70°51'07.9\\\"N 29°13'56.3\\\"E) and has been operational since August 2013 monitoring CO2, CH4, N2O and CO."
            },
            "instrument": {
                "ob_id": 28037,
                "uuid": "963b76fd38f04aec929255271efcf7a2",
                "short_code": "instr",
                "title": "Max Plank Off-Axis Integrated-Cavity Output Spectroscopy (OA-ICOS)",
                "abstract": "Real-time N2O (Nitrous Oxide) and CO (Carbon Monoxide) concentrations are simultaneously and continuously measured using an Off-Axis Integrated-Cavity Output Spectroscopy (OA-ICOS) analyser (Los Gatos Inc).  A Greenhouse Gas Analyser (GGA) using the same fundamental measuring technique was added and placed in series to measure CO2 (Carbon Dioxide) and CH4 (Methane) concentrations. Both devices are configured to sample at a frequency of 1Hz and both have the precision and accuracy to conform to measurement recommendations as defined by Global Atmosphere Watch (GAW).   It is operated by the University of Exeter and the Max Planck Institute for Biogeochemistry at Cape Verde Atmospheric Observatory."
            },
            "relatedTo": {
                "ob_id": 28184,
                "uuid": "e0874965425f4ce6a998c1c0ae6bedaa",
                "short_code": "acq",
                "title": "Kjølnes Atmospheric Observatory (KJN): High-precision long-term atmospheric measurements of greenhouse gases (CO, CO2, N2O and CH4 ) using Off-Axis Integrated-Cavity Output Spectroscopy  (OA-ICOS).",
                "abstract": "Kjølnes Atmospheric Observatory (KJN): High-precision long-term atmospheric measurements of greenhouse gases (CO, CO2, N2O and CH4 ) using Off-Axis Integrated-Cavity Output Spectroscopy  (OA-ICOS)."
            }
        },
        {
            "ob_id": 12279,
            "platform": {
                "ob_id": 25543,
                "uuid": "ff3054702b6e47178e77a6bb1a887440",
                "short_code": "plat",
                "title": "King Edward Point Magnetic Observatory (KEP)",
                "abstract": "The King Edward Point (KEP) magnetic observatory became operational in February 2011. This new observatory occupies the same site as an observatory run by the British Antarctic Survey (BAS) between 1975 - 1982. The observatory is based at King Edward Point, immediately to the north of the BAS / South Georgia government base, at the foot of Mount Duse.\r\n\r\nThis observatory plugs a significant gap in the global network of magnetic observatories allowing better monitoring of the South Atlantic Anomaly and of changes occurring deep within the Earth.\r\n\r\nThe observatory was installed by the British Geological Survey with support from the British Antarctic Survey and The Government of South Georgia and the South Sandwich Islands.\r\n\r\nKing Edward Point magnetic observatory is part of the INTERMAGNET network."
            },
            "instrument": {
                "ob_id": 28239,
                "uuid": "63623413734d48f78229223a02ea49fb",
                "short_code": "instr",
                "title": "British Antarctic Survey: Vaisala RS92 Radiosonde",
                "abstract": "The British Antarctic Survey (BAS) Vaisala RS92 radiosonde sounding system is operated at the King Edward Point launch site.\r\n\r\nVaisala radiosonde systems are used by meteorological organisations all around the world to measure weather in the Earth’s atmosphere, from the boundary layer to the upper atmosphere. The radiosonde is a lightweight, balloon-borne instrument that measures profiles of pressure, temperature and humidity from the ground to approximately 40 km. The radiosonde is equipped with a radio transmitter for sending the measurements securely to the observing station. The user has control over the sounding process by integrating sounding controls, archiving the sounding data and meteorological message creation. For routine soundings the system offers a variety of features and allows the desired balance of manual and automatic control. In addition to the traditional alphanumeric messages, the system software produces the WMO specified BUFR messages. This feature enables users to follow the WMO's recommendation to move from traditional alphanumeric codes to binary BUFR codes."
            },
            "relatedTo": {
                "ob_id": 28242,
                "uuid": "053a9276da8141488642f66369af6eda",
                "short_code": "acq",
                "title": "KEP radiosonde data for SG-Wex",
                "abstract": "KEP radiosonde data for SG-Wex"
            }
        },
        {
            "ob_id": 12280,
            "platform": {
                "ob_id": 1824,
                "uuid": "2a13c66bfad74b98b9cd4201c51de8c1",
                "short_code": "plat",
                "title": "NOAA-16",
                "abstract": "NOAA polar orbiting satellite which was launched on September 21, 2000"
            },
            "instrument": {
                "ob_id": 1817,
                "uuid": "eff26a2de66b4c6b9f71a15e875f52c5",
                "short_code": "instr",
                "title": "Advanced Very High Resolution Radiometer 3 (AVHRR/3)",
                "abstract": "The AVHRR is a radiation-detection imager that can be used for remotely determining cloud cover and the surface temperature. Note that the term surface can mean the surface of the Earth, the upper surfaces of clouds, or the surface of a body of water. This scanning radiometer uses 6 detectors that collect different bands of radiation wavelengths.\n\nThe first AVHRR was a 4-channel radiometer, first carried on TIROS-N (launched October 1978). This was subsequently improved to a 5-channel instrument (AVHRR/2) that was initially carried on NOAA-7 (launched June 1981). The latest instrument version is AVHRR/3, with 6 channels, first carried on NOAA-15 launched in May 1998."
            },
            "relatedTo": {
                "ob_id": 28842,
                "uuid": "748307dfdae24eef936f3a92a72137fd",
                "short_code": "acq",
                "title": "FIDUCEO AVHRR AOT data aquisition for Aerosol Optocal Depth V1.0",
                "abstract": "FIDUCEO AVHRR AOT data aquisition for Aerosol Optocal Depth V1.0"
            }
        },
        {
            "ob_id": 12281,
            "platform": {
                "ob_id": 27174,
                "uuid": "3dba7abe842a4f55b7d27d58cfa6b7ac",
                "short_code": "plat",
                "title": "NOAA-18",
                "abstract": "NOAA (National Oceanic and Atmospheric Administration) polar orbiting satellite which was launched on 20th May, 2005."
            },
            "instrument": {
                "ob_id": 1817,
                "uuid": "eff26a2de66b4c6b9f71a15e875f52c5",
                "short_code": "instr",
                "title": "Advanced Very High Resolution Radiometer 3 (AVHRR/3)",
                "abstract": "The AVHRR is a radiation-detection imager that can be used for remotely determining cloud cover and the surface temperature. Note that the term surface can mean the surface of the Earth, the upper surfaces of clouds, or the surface of a body of water. This scanning radiometer uses 6 detectors that collect different bands of radiation wavelengths.\n\nThe first AVHRR was a 4-channel radiometer, first carried on TIROS-N (launched October 1978). This was subsequently improved to a 5-channel instrument (AVHRR/2) that was initially carried on NOAA-7 (launched June 1981). The latest instrument version is AVHRR/3, with 6 channels, first carried on NOAA-15 launched in May 1998."
            },
            "relatedTo": {
                "ob_id": 28842,
                "uuid": "748307dfdae24eef936f3a92a72137fd",
                "short_code": "acq",
                "title": "FIDUCEO AVHRR AOT data aquisition for Aerosol Optocal Depth V1.0",
                "abstract": "FIDUCEO AVHRR AOT data aquisition for Aerosol Optocal Depth V1.0"
            }
        },
        {
            "ob_id": 12282,
            "platform": {
                "ob_id": 458,
                "uuid": "b6d87ac1455348cd97a4386b38995dbb",
                "short_code": "plat",
                "title": "NIMBUS 7 Satellite",
                "abstract": "The NASA Nimbus 7 research-and-development polar-orbiting satellite served as a stabilized, earth-oriented platform for the testing of advanced systems for sensing and collecting data in the pollution, oceanographic and meteorological disciplines. It was launched on October 24, 1978."
            },
            "instrument": {
                "ob_id": 2607,
                "uuid": "7d9e1c4143054cfbae6f55197227b0a3",
                "short_code": "instr",
                "title": "NIMBUS-7 Coastal Zone Color Scanner (CZCS)",
                "abstract": "The Coastal Zone Color Scanner (CZCS) instrument flew aboard the Nimbus-7 satellite from October 1978 through June 1986."
            },
            "relatedTo": {
                "ob_id": 29896,
                "uuid": "558a56fac72348ab9b244c547955313b",
                "short_code": "acq",
                "title": "Acquisition Process for: CZCS data",
                "abstract": "The acquisition process for the collection of raw imaging data from the CZCS instrument."
            }
        },
        {
            "ob_id": 12283,
            "platform": {
                "ob_id": 29925,
                "uuid": "65c32f4b87db4448bec5f5b52a328cde",
                "short_code": "plat",
                "title": "OrbView-2",
                "abstract": "OrbView 2, also known as SeaStar, is a commercial Earth observation satellite, which operates its SeaWiFS sensor for NASA. On 11 December 2010, after more than 13 years, the communication with the instrument ceased."
            },
            "instrument": {
                "ob_id": 29926,
                "uuid": "35b8af8a77984a8c8839de92c4b89293",
                "short_code": "instr",
                "title": "SeaWiFS",
                "abstract": "Sea-viewing Wide Field-of-view Sensor."
            },
            "relatedTo": {
                "ob_id": 29928,
                "uuid": "91f8d22102f24358980b4660d188cb8c",
                "short_code": "acq",
                "title": "Acquisition process for: SeaWiFS data",
                "abstract": "The acquisition process for the collection of raw imaging data from the SeaWiFS instrument."
            }
        },
        {
            "ob_id": 12284,
            "platform": {
                "ob_id": 27128,
                "uuid": "9c6e8c73f539446ba7a8adef871492a7",
                "short_code": "plat",
                "title": "SMOS",
                "abstract": "The SMOS (Soil Moisture and Ocean Salinity) satellite was launched on Novermber 2009, with the primary mission to monitor ocean salinity and soil moisture."
            },
            "instrument": {
                "ob_id": 27124,
                "uuid": "9b4be0d67030450ca8aebf37cf39500c",
                "short_code": "instr",
                "title": "MIRAS",
                "abstract": "MIRAS (Microwave Imaging Radiometer using Aperture Synthesis) is an European Space Agency instrument flown on the SMOS (Soil Moisture and Ocean Salinity) Satellite.  It measures Ocean Salinity and Soil Moisture."
            },
            "relatedTo": {
                "ob_id": 29943,
                "uuid": "119a7746b29243f5bdb8e329f392bd9f",
                "short_code": "acq",
                "title": "Aquistion process for CCI Sea Surface Salinity data",
                "abstract": "The ESA CCI Climate Change Initiate Sea Surface Salinity project has derived salinity data from the SMOS, SMAP and Aquarius Satellite instruments."
            }
        },
        {
            "ob_id": 12285,
            "platform": {
                "ob_id": 29941,
                "uuid": "2b126b39dbb64c0681f12b68f2308fee",
                "short_code": "plat",
                "title": "SMAP",
                "abstract": "The Soil Moisture Active-Passive (SMAP) satelliteis a NASA satellite launched in 2015."
            },
            "instrument": {
                "ob_id": 29938,
                "uuid": "e050ad22e3b943f9a5f1563a1e6fb82c",
                "short_code": "instr",
                "title": "SMAP",
                "abstract": "The Soil Moisture Active Passive instrument is a microwave radiometer flown on the NASA SMAP satellite."
            },
            "relatedTo": {
                "ob_id": 29943,
                "uuid": "119a7746b29243f5bdb8e329f392bd9f",
                "short_code": "acq",
                "title": "Aquistion process for CCI Sea Surface Salinity data",
                "abstract": "The ESA CCI Climate Change Initiate Sea Surface Salinity project has derived salinity data from the SMOS, SMAP and Aquarius Satellite instruments."
            }
        },
        {
            "ob_id": 12286,
            "platform": {
                "ob_id": 29940,
                "uuid": "a55f223286b34dd5a0df0a471ff4c07b",
                "short_code": "plat",
                "title": "SAC-D",
                "abstract": "The Satélite de Aplicaciones Cientificas - D (SAC-D) was a collaboration between the space agencies of Argentina (CONAS) and the United States (NASA), with participation from Brazil, Canada, France and Italy ."
            },
            "instrument": {
                "ob_id": 29939,
                "uuid": "c217abe1355e4a7db2e4bb23782edafb",
                "short_code": "instr",
                "title": "Aquarius",
                "abstract": "The Aquarius Instrument is a passive microwave radiometer for measuring ocean salinity and soil moisture.   It has been flown the SAC-D satellite (Satélite de Aplicaciones Cientificas - D).   The Aquarius / SAC-D mission is a joint mission between NASA and the Argentinian Space Agency (CONAE)."
            },
            "relatedTo": {
                "ob_id": 29943,
                "uuid": "119a7746b29243f5bdb8e329f392bd9f",
                "short_code": "acq",
                "title": "Aquistion process for CCI Sea Surface Salinity data",
                "abstract": "The ESA CCI Climate Change Initiate Sea Surface Salinity project has derived salinity data from the SMOS, SMAP and Aquarius Satellite instruments."
            }
        },
        {
            "ob_id": 12287,
            "platform": {
                "ob_id": 12319,
                "uuid": "b6a54b30cf1f45d79e08117ccabeceb6",
                "short_code": "plat",
                "title": "Sentinel 1A",
                "abstract": "Sentinel 1A is the first of the European Space Agency (ESA) Sentinel series. It was launched on 3rd April 2014."
            },
            "instrument": {
                "ob_id": 12313,
                "uuid": "0604b6ac4fb24640895c84a25edfd078",
                "short_code": "instr",
                "title": "Sentinel 1 Synthetic Aperture Radar (SAR)",
                "abstract": "The  C-band Synthetic Aperture Radar (SAR) flown on the Sentinel 1 series of satellites is an instrument providing high resolution all-weather day and night radar coverage of the Earth's surface.\r\nSentinel 1A was launched on 3rd April 2014 and Sentinel 1B was launched on 25th April 2016. This instrument has four acquisition modes; Stripmap (SM), Interferometric Wide Swath (IW), Extra Wide Swath (EW), and Wave (WV)."
            },
            "relatedTo": {
                "ob_id": 29956,
                "uuid": "c8b2caa776da4515833a1ba6aa3ddc0e",
                "short_code": "acq",
                "title": "CCI Biomass",
                "abstract": "CCI Biomass"
            }
        },
        {
            "ob_id": 12288,
            "platform": {
                "ob_id": 29959,
                "uuid": "d367f0c185a84677a52487304474a3aa",
                "short_code": "plat",
                "title": "ALOS-2",
                "abstract": "The Advanced Land Observing Satellite -2 (ALOS-2) is an Earth Observation satellite operated by JAXA and is the second instrument in the ALOS programme of satellites.   It carries two instruments: PALSAR-2 (Phased-Array L-band Synthetic Aperture Radar - 2 )  and CIRC (Compact Infrared Camera)"
            },
            "instrument": {
                "ob_id": 29958,
                "uuid": "8030695806b544f3948439758ea9b38f",
                "short_code": "instr",
                "title": "PALSAR-2",
                "abstract": "The Phased Array type-L band Synthetic Aperture Radar -2 (PALSAR-2) is an active microwave sensor using L-band frequency and which produces various products of different resolutions and performance. PALSAR-2 is flown on board the Japanese earth observation Advanced Land Observing Satellite 2 (ALOS -2) and was developed by the Japanese Aerospace Exploration Agency (JAXA). PALSAR-2 data can be acquired during day or night, increasing the temporal coverage of data for a particular spatial extent. PALSAR-2 is capable of detailed, all-weather, day and night observations and repeat-pass interferometry."
            },
            "relatedTo": {
                "ob_id": 29956,
                "uuid": "c8b2caa776da4515833a1ba6aa3ddc0e",
                "short_code": "acq",
                "title": "CCI Biomass",
                "abstract": "CCI Biomass"
            }
        },
        {
            "ob_id": 12289,
            "platform": {
                "ob_id": 24927,
                "uuid": "a8aa0f0e0a0745eb900bd41c37592212",
                "short_code": "plat",
                "title": "Swedish Maritime Administration Icebreaker Oden",
                "abstract": "The polar classed Icebreaker Oden (call sign SMLQ) is designed as a combined escort icebreaker and research vessel. She was the first non-nuclear icebreaker at the North Pole in 1991, with a total of seven visits. Between the years 2006-2011 she conducted five successful cruises to Antarctica. In the course of time, Oden has been upgraded and fitted with advanced scientific equipment. It was also deployed during the 2014 Arctic Cloud Summer Expedition (ACSE)."
            },
            "instrument": {
                "ob_id": 3054,
                "uuid": "86569f5888ec4e06a9c8bb000126c0b9",
                "short_code": "instr",
                "title": "NCAS AMF: Vaisala Radiosonde Unit 2",
                "abstract": "The National Centre for Atmospheric Science's Atmospheric Measurement Facility (NCAS AMF) operate two radiosonde sounding systems: unit one is situated at the University of Manchester and unit two at the University of Leeds, both compatible with the Vaisala RS92 sonde family and support the extended sondes recommended by Vaisala. Both systems are 400 MHz variants.\r\n\r\nAlthough now designated as NCAS AMF instruments they have each had previous designations with this unit previously been known as the \"University of Leeds: Vaisala Radiosonde\" and represented by \"leeds-radiosonde\" in filenames.\r\n\r\nVaisala radiosonde systems are used by meteorological organizations all around the world to measure weather in the Earth’s atmosphere, from the boundary layer to the upper atmosphere. The radiosonde is a lightweight, balloon-borne instrument that measures profiles of pressure, temperature and humidity from the ground to approximately 40 km. The radiosonde is equipped with a radio transmitter for sending the measurements securely to the observing station. The user has control over the sounding process by integrating sounding controls, archiving the sounding data and meteorological message creation. For routine soundings the system offers a variety of features and allows the desired balance of manual and automatic control. In addition to the traditional alphanumeric messages, the system software produces the WMO specified BUFR messages. This feature enables users to follow the WMO's recommendation to move from traditional alphanumeric codes to binary BUFR codes.\r\n\r\nThis record also records the present and previous instrument scientists responsible for the equipment (recorded here as \"operators\") for historic purposes with the current instrument scientist given last. It is possible that other operators may use the equipment from time to time and these should be recorded as dataset authors for each associated datasets in the archive."
            },
            "relatedTo": {
                "ob_id": 29976,
                "uuid": "e62a7777331f4906a34cbbc1ccec5460",
                "short_code": "acq",
                "title": "Acquisition for: Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): composite temperature, humidity and wind profiles and derived variables from the NCAS AMF radiosondes launched from Icebreaker Oden",
                "abstract": "Acquisition for: Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): composite temperature, humidity and wind profiles and derived variables from the NCAS AMF radiosondes launched from Icebreaker Oden"
            }
        },
        {
            "ob_id": 12290,
            "platform": {
                "ob_id": 26503,
                "uuid": "e494bef9ef884794a65a341e58205eb2",
                "short_code": "plat",
                "title": "Alliance Ship",
                "abstract": "Alliance  is a research ship. The 93 meters, 3,180 t NATO ship NRV ALLIANCE was designed in the mid 80’s as a quiet acoustic research platform. It is capable of operating in all oceans strategically important to NATO nations. ALLIANCE enables scientists and engineers from the Centre and partner nations to conduct a wide range of experiments. The ship is equipped with modern scientific instruments, a sophisticated navigation system, and its deck comprises of a vast array of winches (some fitted and some removable), heavy cranes, a lateral frame and a stern U-frame (including a large 4 drum main tow winch for large arrays). This variety of deck equipment allows a large variety of launch and recovery of scientific and engineering sensors, oceanographic instruments, autonomous vehicles and tethered devices."
            },
            "instrument": {
                "ob_id": 29986,
                "uuid": "8d7472c544e846c988cb49b3d2358eb9",
                "short_code": "instr",
                "title": "University of Bergen: Windcube lidar wind profiler",
                "abstract": "This is a lidar wind profiler built by leosphere and it belongs to and was operated by University of Bergen"
            },
            "relatedTo": {
                "ob_id": 29985,
                "uuid": "e94feeab305744b987ac6a4fdd203dc6",
                "short_code": "acq",
                "title": "Acquisition for: Iceland Greenland Seas Project (IGP): three dimensional wind profile measurements from the University of Bergen Windcube V2 pulsed Lidar on board the NATO Research Vessel Alliance",
                "abstract": "Acquisition for: Iceland Greenland Seas Project (IGP): three dimensional wind profile measurements from the University of Bergen Windcube V2 pulsed Lidar on board the NATO Research Vessel Alliance"
            }
        },
        {
            "ob_id": 12291,
            "platform": {
                "ob_id": 27128,
                "uuid": "9c6e8c73f539446ba7a8adef871492a7",
                "short_code": "plat",
                "title": "SMOS",
                "abstract": "The SMOS (Soil Moisture and Ocean Salinity) satellite was launched on Novermber 2009, with the primary mission to monitor ocean salinity and soil moisture."
            },
            "instrument": {
                "ob_id": 27124,
                "uuid": "9b4be0d67030450ca8aebf37cf39500c",
                "short_code": "instr",
                "title": "MIRAS",
                "abstract": "MIRAS (Microwave Imaging Radiometer using Aperture Synthesis) is an European Space Agency instrument flown on the SMOS (Soil Moisture and Ocean Salinity) Satellite.  It measures Ocean Salinity and Soil Moisture."
            },
            "relatedTo": {
                "ob_id": 29991,
                "uuid": "94af481296114c0a97e41d49a232ff69",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20191218145448__ Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v4.4",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 and MIRAS)"
            }
        },
        {
            "ob_id": 12292,
            "platform": {
                "ob_id": 27130,
                "uuid": "526c6fb02e094d049d367aaa4f79e8d1",
                "short_code": "plat",
                "title": "Coriolis",
                "abstract": "The Coriolis satellite is flown by NASA and the US Department of Defence, with a primary mission to provide observations of the sea-surface wind.   It carries two instruments: WindSat and SMEI (Solar Mass Ejection Imager)"
            },
            "instrument": {
                "ob_id": 27125,
                "uuid": "10f4aca379f84e0cae56392a85604469",
                "short_code": "instr",
                "title": "WindSat",
                "abstract": "WindSat is a passive microwave radiometer flown on the Coriolis Satellite by the US Department of Defence since 2003."
            },
            "relatedTo": {
                "ob_id": 29991,
                "uuid": "94af481296114c0a97e41d49a232ff69",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20191218145448__ Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v4.4",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 and MIRAS)"
            }
        },
        {
            "ob_id": 12293,
            "platform": {
                "ob_id": 25273,
                "uuid": "f10d619f7b9f4dbab792dcc1ab9dbb68",
                "short_code": "plat",
                "title": "GCOM-W (Global Change Observation Mission for Water)",
                "abstract": "The Global Change Observation Mission for Water (GCOM-W) is a series of three satellites flown by the Japanese Space Agency (JAXA), addressing multi-purpose MW imagery for ocean, land and precipitation.  It is part of their Global Change Observation Mission (GCOM).\r\nThe satellites exploit sun-synchronous orbits around 13:30, coordinated with that of POES satellites, Suomi-NPP and JPSS."
            },
            "instrument": {
                "ob_id": 25272,
                "uuid": "a6002da7c0954ce0aa146c1b24877a0a",
                "short_code": "instr",
                "title": "AMSR-2",
                "abstract": "Advanced Microwave Scanning Radiometer -2, flying on the Global Change Observation Mission (GCOM) series of satellites flown by JAXA"
            },
            "relatedTo": {
                "ob_id": 29991,
                "uuid": "94af481296114c0a97e41d49a232ff69",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20191218145448__ Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v4.4",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 and MIRAS)"
            }
        },
        {
            "ob_id": 12294,
            "platform": {
                "ob_id": 10906,
                "uuid": "5a1076bffc8c4c5d8a2ff3a4cfb29846",
                "short_code": "plat",
                "title": "Aqua Satellite, part of the Earth Observation System Afternoon Constellation (EOS-PM)",
                "abstract": "Aqua, launched on 4th April 2002, is a polar-orbiting satellite within the Afternoon Constellation (A-Train) that have equator crossings around 13:30 and 01:30 under NASA's Earth Obseration System (EOS). The satellite carries Atmospheric Infrared Sounder (AIRS), Advanced Microwave Sounding Unit (AMSU-A), Humidity Sounder for Brazil (HSB), Advanced Microwave Scanning Radiometer for EOS (AMSR-E), Moderate-Resolution Imaging Spectroradiometer (MODIS) and Clouds and the Earth's Radiant Energy System (CERES), and these collect data on the Earth's atmospheric conditions, snow and ice, sea surface temperature and ocean productivity, and soil moisture.   Aqua was the first member launched of a group of satellites termed the Afternoon Constellation, or sometimes the A-Train. "
            },
            "instrument": {
                "ob_id": 14485,
                "uuid": "77dd26fc341a440b85a98fe95b1976f8",
                "short_code": "instr",
                "title": "AMSR-E",
                "abstract": "Advanced Microwave Scanning Radiometer for EOS"
            },
            "relatedTo": {
                "ob_id": 29991,
                "uuid": "94af481296114c0a97e41d49a232ff69",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20191218145448__ Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v4.4",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 and MIRAS)"
            }
        },
        {
            "ob_id": 12295,
            "platform": {
                "ob_id": 27135,
                "uuid": "8afe985a2f3f4b15aaa52df6119c0f27",
                "short_code": "plat",
                "title": "TRMM",
                "abstract": "The Tropical Rainfall Measuring Mission (TRMM) is a NASA and JAXA satellite that flew between 1997 and 2015.  It's primary mission was to measure precipitation."
            },
            "instrument": {
                "ob_id": 27126,
                "uuid": "9173171ba44845e9a873e21b4dee19e2",
                "short_code": "instr",
                "title": "TMI",
                "abstract": "TMI (TRMM  Microwave Imager) is a multi-purpose microwave imager flying on the TRMM (Tropical Rainfall Measuring Mission)."
            },
            "relatedTo": {
                "ob_id": 29991,
                "uuid": "94af481296114c0a97e41d49a232ff69",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20191218145448__ Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v4.4",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 and MIRAS)"
            }
        },
        {
            "ob_id": 12296,
            "platform": {
                "ob_id": 2629,
                "uuid": "9f1b0a2380cc47919b201880e0fee6de",
                "short_code": "plat",
                "title": "Defense Meteorological Satellite Program (DMSP) Satellites",
                "abstract": "DMSP satellites are used for strategic and tactical weather prediction to aid the U.S. military in planning operations at sea, on land and in the air. Equipped with a sophisticated sensor suite that can image visible and infrared cloud cover and measure precipitation, surface temperature, and soil moisture, the satellite collects specialized global meteorological, oceanographic, and solar-geophysical information in all weather conditions. The DMSP constellation comprises two spacecraft in near-polar orbits, C3 (command, control and communications), user terminals and weather centers."
            },
            "instrument": {
                "ob_id": 2630,
                "uuid": "54f897597ec04c09b01095eb05c7419e",
                "short_code": "instr",
                "title": "Special Sensor Microwave / Imager (SSM/I)",
                "abstract": "The SSM/I is a seven-channel, four frequency, linearly-polarized, passive microwave radiometric system which measures atmospheric, ocean and terrain microwave brightness temperatures at 19.35, 22.235, 37.0 and 85.5 GHz. The data are used to obtain synoptic maps of critical atmospheric, oceanographic and selected land parameters on a global scale."
            },
            "relatedTo": {
                "ob_id": 29991,
                "uuid": "94af481296114c0a97e41d49a232ff69",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20191218145448__ Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v4.4",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 and MIRAS)"
            }
        },
        {
            "ob_id": 12297,
            "platform": {
                "ob_id": 458,
                "uuid": "b6d87ac1455348cd97a4386b38995dbb",
                "short_code": "plat",
                "title": "NIMBUS 7 Satellite",
                "abstract": "The NASA Nimbus 7 research-and-development polar-orbiting satellite served as a stabilized, earth-oriented platform for the testing of advanced systems for sensing and collecting data in the pollution, oceanographic and meteorological disciplines. It was launched on October 24, 1978."
            },
            "instrument": {
                "ob_id": 2636,
                "uuid": "1578228cc3cf4b9fba0b88c61b58800b",
                "short_code": "instr",
                "title": "Scanning Multichannel Microwave Radiometer (SMMR)",
                "abstract": "The Scanning Multichannel Microwave Radiometer operated on NASA's Nimbus-7 satellite for more than eight years, from 26 October 1978 to 20 August 1987, transmitting data every other day. Intended to obtain ocean circulation parameters such as sea surface temperatures, low altitude winds, water vapor and cloud liquid water content on an all-weather basis, the SMMR is a ten channel instrument capable of receiving both horizontally and vertically polarized radiation. A parabolic antenna 79 cm in diameter reflected microwave emissions into a five-frequency feed horn. The antenna beam maintained a constant nadir angle of 42 degrees, resulting in an incidence angle of 50.3 degrees at Earth's surface. The antenna was forward viewing and rotated equally +/- 25 degrees about the satellite subtrack. The 50 degree scan provided a 780 km swath of the Earth's surface. Scan period was 4.096 seconds."
            },
            "relatedTo": {
                "ob_id": 29991,
                "uuid": "94af481296114c0a97e41d49a232ff69",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20191218145448__ Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v4.4",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 and MIRAS)"
            }
        },
        {
            "ob_id": 12298,
            "platform": {
                "ob_id": 8207,
                "uuid": "3f2dbe69fe4c40ee9e1e8be87e15a1d5",
                "short_code": "plat",
                "title": "Metop-A",
                "abstract": "Metop-A, launched on 19 October 2006, represents the first in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS). Metop-A is Europe's first polar-orbiting meteorological satellite"
            },
            "instrument": {
                "ob_id": 27121,
                "uuid": "ca133e0771514003a9e7c2462c1b363c",
                "short_code": "instr",
                "title": "ASCAT",
                "abstract": "ASCAT (Advanced Scatterometer)  is a C Band (2.55 GHz) Scatterometer flown on the Metop series of satellites.  It measures the sea surface wind vecotr and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 29991,
                "uuid": "94af481296114c0a97e41d49a232ff69",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20191218145448__ Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v4.4",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 and MIRAS)"
            }
        },
        {
            "ob_id": 12299,
            "platform": {
                "ob_id": 8299,
                "uuid": "84a6355ac58249cc8c636e77a243c86a",
                "short_code": "plat",
                "title": "Metop-B",
                "abstract": "Metop-B, launched on the 17th September 2012, is the second in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS)."
            },
            "instrument": {
                "ob_id": 27121,
                "uuid": "ca133e0771514003a9e7c2462c1b363c",
                "short_code": "instr",
                "title": "ASCAT",
                "abstract": "ASCAT (Advanced Scatterometer)  is a C Band (2.55 GHz) Scatterometer flown on the Metop series of satellites.  It measures the sea surface wind vecotr and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 29991,
                "uuid": "94af481296114c0a97e41d49a232ff69",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20191218145448__ Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v4.4",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 and MIRAS)"
            }
        },
        {
            "ob_id": 12300,
            "platform": {
                "ob_id": 7805,
                "uuid": "d21630e98aa74a4f8406743b74e5d076",
                "short_code": "plat",
                "title": "ERS-1",
                "abstract": "The European Remote Sensing satellite 1 (ERS1) was launched on 17th July 1991 and was the first flight of the RSA ERS program.  The payload included the ATSR, AMU-SAR , AMI-SCAT, LRR PRARE and RA instruments.  End of mission for ERS1 was 10th March 2000."
            },
            "instrument": {
                "ob_id": 27122,
                "uuid": "7b488736a173477689480990d5b38aa9",
                "short_code": "instr",
                "title": "AMI-SCAT",
                "abstract": "AMI-SCAT (Active Microwave Instrument - Scatterometer) is a C-band (5.3 GHz) scatterometer flying on the ERS-1 and ERS-2 satellites.  It measures the sea surface wind vector and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 29991,
                "uuid": "94af481296114c0a97e41d49a232ff69",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20191218145448__ Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v4.4",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 and MIRAS)"
            }
        },
        {
            "ob_id": 12301,
            "platform": {
                "ob_id": 7813,
                "uuid": "8ee876e1ea644ed7a81d4e3536133fa0",
                "short_code": "plat",
                "title": "European Remote Sensing satellite 2 - ERS-2",
                "abstract": "ESA's two European Remote Sensing (ERS) satellites, ERS-1 and –2, were launched into the same orbit in 1991 and 1995 respectively. Their payloads included a synthetic aperture imaging radar, radar altimeter and instruments to measure ocean surface temperature and wind fields.\r\n\r\nERS-2 added an additional sensor for atmospheric ozone monitoring. The two satellites acquired a combined data set extending over two decades.\r\n\r\nThe ERS-2 satellite was retired on 05 September 2011."
            },
            "instrument": {
                "ob_id": 27122,
                "uuid": "7b488736a173477689480990d5b38aa9",
                "short_code": "instr",
                "title": "AMI-SCAT",
                "abstract": "AMI-SCAT (Active Microwave Instrument - Scatterometer) is a C-band (5.3 GHz) scatterometer flying on the ERS-1 and ERS-2 satellites.  It measures the sea surface wind vector and large-scale soil moisture."
            },
            "relatedTo": {
                "ob_id": 29991,
                "uuid": "94af481296114c0a97e41d49a232ff69",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20191218145448__ Acquistion process for the ESA Soil Moisture Climate Change Initiative Combined product, v4.4",
                "abstract": "The ESA Climate Change Initiative Combined product has been derived from data from both active (AMI-SCAT, ASCAT) and passive satellite instruments  (SMMR, SSM/I, TMI, AMSR-E, WindSat, AMSR2 and MIRAS)"
            }
        },
        {
            "ob_id": 12302,
            "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": 25990,
                "uuid": "267d04e7112f4340ad53c4e41b79d28b",
                "short_code": "instr",
                "title": "Birmingham: Dionex IC 2100 Ion Chromatography (IC)",
                "abstract": "Dionex IC 2100 Ion chromatography is a chromatography process that separates ions and polar molecules based on their affinity to the ion exchanger. It works on almost any kind of charged molecule—including large proteins, small nucleotides, and amino acids."
            },
            "relatedTo": {
                "ob_id": 29997,
                "uuid": "6cf21f0e930f45d6b53d15fcf9902d46",
                "short_code": "acq",
                "title": "Acquisition for: Si-SOA study_inorganic ions data set 2018-2019",
                "abstract": "Acquisition for: Si-SOA study_inorganic ions data set 2018-2019"
            }
        },
        {
            "ob_id": 12303,
            "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": 25989,
                "uuid": "2a6b5533bb624d90ab8bf76d577162ad",
                "short_code": "instr",
                "title": "Birmingham: Inductively Coupled Plasma Mass Spectrometry (ICP-MS)",
                "abstract": "Inductively Coupled Plasma Mass Spectrometry or ICP-MS is an analytical technique used for elemental determinations. We extract the metals from filters using HCl/HNO3, then the extract was diluted and analyzed by ICP-MS. An ICP-MS combines a high-temperature ICP (Inductively Coupled Plasma) source with a mass spectrometer. The ICP source converts the atoms of the elements in the sample to ions. These ions are then separated and detected by the mass spectrometer."
            },
            "relatedTo": {
                "ob_id": 30028,
                "uuid": "af61fe4432f64e8a818392d2e8c58b2f",
                "short_code": "acq",
                "title": "Si-SOA: inductively coupled plasma mass spectrometry (ICP-MS) PM2.5 measurements taken from IAP-Beijing site",
                "abstract": "Si-SOA: inductively coupled plasma mass spectrometry (ICP-MS) PM2.5 measurements taken from IAP-Beijing site"
            }
        },
        {
            "ob_id": 12304,
            "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": 30031,
                "uuid": "19eb34b64523452fb2d3d82453cfe924",
                "short_code": "instr",
                "title": "Birmingham: Inductively coupled plasma - optical emission spectrometry (ICP-OES)",
                "abstract": "Inductively coupled plasma - optical emission spectrometry (ICP-OES) (model: Optima 8000; PerkinElmer) is located in University of Birmingham WG1 laboratory. \r\n\r\nICP-OES is a trace-level, elemental analysis technique that uses the emission spectra of a sample to identify, and quantify the elements present. Samples are introduced into the plasma in a process that desolvates, ionises, and excites them."
            },
            "relatedTo": {
                "ob_id": 30032,
                "uuid": "fac3f828bc834a5bb84cb4b0433ee5b4",
                "short_code": "acq",
                "title": "Si-SOA: coupled plasma - optical emission spectrometry (ICP-OES) PM2.5 measurements taken from IAP-Beijing site",
                "abstract": "Si-SOA: coupled plasma - optical emission spectrometry (ICP-OES) PM2.5 measurements taken from IAP-Beijing site"
            }
        },
        {
            "ob_id": 12305,
            "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": 30035,
                "uuid": "4b4039530c7947f6ad71983a5dc72bc1",
                "short_code": "instr",
                "title": "Birmingham: ultraviolet–visible spectrophotometry (UV-Vis)",
                "abstract": "The UV-Vis instrument (model: 6800UV / Vis. Spectrophotometer; JENWAY) is located in University of Birmingham WG1 laboratory."
            },
            "relatedTo": {
                "ob_id": 30036,
                "uuid": "aa7b225b927b43aabb94b3600a0b4e68",
                "short_code": "acq",
                "title": "Si-SOA: ultraviolet–visible spectrophotometry (UV-Vis) PM2.5 measurements taken from IAP-Beijing site",
                "abstract": "Si-SOA: ultraviolet–visible spectrophotometry (UV-Vis) PM2.5 measurements taken from IAP-Beijing site"
            }
        },
        {
            "ob_id": 12306,
            "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": 25988,
                "uuid": "2342c7b6f47144edb78b6986970b6f6f",
                "short_code": "instr",
                "title": "Birmingham: X-ray fluorescence (XRF)",
                "abstract": "WD-XRF instrument (Tiger Bruker S8). Principal:The basis of X-ray fluorescence spectrometry is the interaction of X-ray photons from a separate excitation source with atoms of the elements of interest found in the sample (filter deposit). When these excitation photons interact with the atoms in the sample, the photons cause the ejection of inner shell electrons. Outer shell electrons then fall into these vacancies. These transitions result in emission of Xrays characteristic of the element. The energy of the characteristic X-ray is equal to the difference in the electron binding energies of the two electron shells involved in the transition. Because the electron binding energies are a function of the atomic number, the energy of the X-ray is characteristic of the element."
            },
            "relatedTo": {
                "ob_id": 30039,
                "uuid": "1967c2c9184643138adc3f6d000c73bd",
                "short_code": "acq",
                "title": "Si-SOA: X-ray Fluorescence Spectrometer (XRF) PM2.5 measurements taken from IAP-Beijing site",
                "abstract": "Si-SOA: X-ray Fluorescence Spectrometer (XRF) PM2.5 measurements taken from IAP-Beijing site"
            }
        },
        {
            "ob_id": 12307,
            "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": 30043,
                "uuid": "f09b2f2da4994897b217afa3f41b47af",
                "short_code": "instr",
                "title": "Cambrige: LTQ Orbitrap Velos",
                "abstract": "LTQ Orbitrap Velos ultrahigh resolution mass spectrometer located at the Department of  Chemistry of the University of Cambridge"
            },
            "relatedTo": {
                "ob_id": 30044,
                "uuid": "60a9675fdb2e4b6190b566b773a060c6",
                "short_code": "acq",
                "title": "APHH: Direct infusion ultrahigh resolution mass spectrometry measurements made at the IAP-Beijing site during the summer and winter campaigns",
                "abstract": "APHH: Direct infusion ultrahigh resolution mass spectrometry measurements made at the IAP-Beijing site during the summer and winter campaigns"
            }
        },
        {
            "ob_id": 12308,
            "platform": {
                "ob_id": 30097,
                "uuid": "8afc6e3702f946daa89e2af71632406a",
                "short_code": "plat",
                "title": "Wytham Woods",
                "abstract": "Wytham Woods, an ancient woodland in the UK"
            },
            "instrument": {
                "ob_id": 30096,
                "uuid": "366d60e310f444489331cc1698642dec",
                "short_code": "instr",
                "title": "iDarac gas chromatograph",
                "abstract": "Isoprene abundances were measured using the iDirac (Bolas et al., Atm. Meas. Tech., 2020), a custom-built portable gas chromatograph with photo-ionisation detection (GC-PID). The instrument is designed for continuous and autonomous operation, with a Raspberry Pi/Arduino-controlled system, low power usage (12 W) and low gas consumption. Frequent calibration runs (typically every 5 hours) ensured maximum accuracy of the measurements. The limit of detection is 40 ppt (signal to noise of 3), with 10% precision.\r\n\r\nAir temperature was monitored every 2 minutes by four EasyLog probes (EL-USB-2-LCD & EL-USB-2, Lascar Ltd).\r\n\r\nPhotosythetically Active Radiation (PAR) was monitored using 4 SQ-110 Quantum Apogee sensors (Campbell Scientific)"
            },
            "relatedTo": {
                "ob_id": 30098,
                "uuid": "a443dee426114fefb97c7dce738b916e",
                "short_code": "acq",
                "title": "Biodiversity and Land Use Impacts on Tropical Forest Ecosystem Function (BALI): Isoprene concentration measurements at Wytham Woods (UK) during the summer of 2018",
                "abstract": "Biodiversity and Land Use Impacts on Tropical Forest Ecosystem Function (BALI): Isoprene concentration measurements at Wytham Woods (UK) during the summer of 2018"
            }
        },
        {
            "ob_id": 12309,
            "platform": {
                "ob_id": 24927,
                "uuid": "a8aa0f0e0a0745eb900bd41c37592212",
                "short_code": "plat",
                "title": "Swedish Maritime Administration Icebreaker Oden",
                "abstract": "The polar classed Icebreaker Oden (call sign SMLQ) is designed as a combined escort icebreaker and research vessel. She was the first non-nuclear icebreaker at the North Pole in 1991, with a total of seven visits. Between the years 2006-2011 she conducted five successful cruises to Antarctica. In the course of time, Oden has been upgraded and fitted with advanced scientific equipment. It was also deployed during the 2014 Arctic Cloud Summer Expedition (ACSE)."
            },
            "instrument": {
                "ob_id": 24938,
                "uuid": "2a511f1d9ab649469c1acad69b03c5d0",
                "short_code": "instr",
                "title": "University of Leeds: Heitronics KT15 IR temperature sensor 1",
                "abstract": "The University of Leeds Heitronics KT15 IR temperature sensor (number 1) is a digital, compact, programmable and universally applicable radiation pyrometer series with comprehensive and flexible functions for industrial temperature monitoring and control. It measures surface temperature remotely from infra red radiation.\r\n\r\nThe KT15.85 IIP\tmodel is able to measure between -25 and 200 °C.\r\n\r\nData are measured and outputted at 1Hz.\r\n\r\nIt features: \r\n - Extreme high stability due to Chopped Radiation Method\r\n - Very high resolution 0.03 °C\r\n - Fast response times from 5 ms on low temperatures\r\n - Very high linearization accuracy (0.02K)\r\n - Fields-of-view from 0.7 mm at low temperatures allow high optical resolutions\r\n - Permanent self-monitoring routines ensure a reliable operation\r\n - Integrated calibration routine allows for fast and reliable control of the device."
            },
            "relatedTo": {
                "ob_id": 30101,
                "uuid": "6327369a61284e2fb03c2f0ddafe941d",
                "short_code": "acq",
                "title": "Acquisition for: Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): surface temperature measurements from the University of Leeds Heitronics KT15.85 infra red radiative temperature sensor from an ice-floe site",
                "abstract": "Acquisition for: Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): surface temperature measurements from the University of Leeds Heitronics KT15.85 infra red radiative temperature sensor from an ice-floe site"
            }
        },
        {
            "ob_id": 12310,
            "platform": {
                "ob_id": 24927,
                "uuid": "a8aa0f0e0a0745eb900bd41c37592212",
                "short_code": "plat",
                "title": "Swedish Maritime Administration Icebreaker Oden",
                "abstract": "The polar classed Icebreaker Oden (call sign SMLQ) is designed as a combined escort icebreaker and research vessel. She was the first non-nuclear icebreaker at the North Pole in 1991, with a total of seven visits. Between the years 2006-2011 she conducted five successful cruises to Antarctica. In the course of time, Oden has been upgraded and fitted with advanced scientific equipment. It was also deployed during the 2014 Arctic Cloud Summer Expedition (ACSE)."
            },
            "instrument": {
                "ob_id": 25998,
                "uuid": "d35f8ddefa8442d9b63883f05aa40057",
                "short_code": "instr",
                "title": "NCAS AMF: Halo Doppler Lidar unit 1",
                "abstract": "NCAS AMF: Halo Doppler Lidar unit 1"
            },
            "relatedTo": {
                "ob_id": 30105,
                "uuid": "f5f3f1452f724caca7a9d613b34d5584",
                "short_code": "acq",
                "title": "Acquisition for: Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): composite lidar wind profile data from the NCAS AMF Halo Doppler lidar on board Icebreaker Oden",
                "abstract": "Acquisition for: Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): composite lidar wind profile data from the NCAS AMF Halo Doppler lidar on board Icebreaker Oden"
            }
        },
        {
            "ob_id": 12311,
            "platform": {
                "ob_id": 24866,
                "uuid": "2ca4d30810cd4b98a71b1993598434af",
                "short_code": "plat",
                "title": "Penlee Point Atmospheric Observatory",
                "abstract": "The Penlee Point Atmospheric Obervaory, created by the Plymouth Marine Laboratory, PML in order to carry out long-term operations aurrounding the ineractions between the ocean and atmosphere. \r\nThe operations are attended to and maintained once every 1-2 weeks."
            },
            "instrument": {
                "ob_id": 30123,
                "uuid": "f9226cf7ef074f09b66b027b9615980c",
                "short_code": "instr",
                "title": "Eco Physics Ozone CLD",
                "abstract": "10 Hz ozone chemiluminescence detector, adapted from an Eco Physics NOx detector. A cylinder supplies 2% NO in N2 which reacts with O3 to form NO2 in an excited state. On relaxation, a photon is emitted, which is amplified and detected using a photomultiplier tube."
            },
            "relatedTo": {
                "ob_id": 30122,
                "uuid": "4f1f390f18884a42a06999adf171f2e2",
                "short_code": "acq",
                "title": "Acquisition for: Ozone eddy covariance measurements at Penlee Point Atmospheric Observatory (PPAO), Apr-May 2018",
                "abstract": "Acquisition for: Ozone eddy covariance measurements at Penlee Point Atmospheric Observatory (PPAO), Apr-May 2018"
            }
        },
        {
            "ob_id": 12312,
            "platform": {
                "ob_id": 24927,
                "uuid": "a8aa0f0e0a0745eb900bd41c37592212",
                "short_code": "plat",
                "title": "Swedish Maritime Administration Icebreaker Oden",
                "abstract": "The polar classed Icebreaker Oden (call sign SMLQ) is designed as a combined escort icebreaker and research vessel. She was the first non-nuclear icebreaker at the North Pole in 1991, with a total of seven visits. Between the years 2006-2011 she conducted five successful cruises to Antarctica. In the course of time, Oden has been upgraded and fitted with advanced scientific equipment. It was also deployed during the 2014 Arctic Cloud Summer Expedition (ACSE)."
            },
            "instrument": {
                "ob_id": 7614,
                "uuid": "8119f25d0570407c925043f603d0b54c",
                "short_code": "instr",
                "title": "Leeds: Forward Scattering Spectroscopy Probe (FSSP)",
                "abstract": "A forward scattering spectrometer probe (FSSP) is an optical particle counter, suitable for counting and sizing particles in the size range of 0.5 - 47 micron diameter."
            },
            "relatedTo": {
                "ob_id": 30134,
                "uuid": "2b65eb0bb1674b30bdb93634d235725a",
                "short_code": "acq",
                "title": "Acquisition for: Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): particle concentration and particle size distribution from the University of Leeds FSSP on board Icebreaker Oden",
                "abstract": "Acquisition for: Microbiology-Ocean-Cloud Coupling in the High Arctic (MOCCHA): particle concentration and particle size distribution from the University of Leeds FSSP on board Icebreaker Oden"
            }
        },
        {
            "ob_id": 12313,
            "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": 30174,
                "uuid": "bfa9cf69515f4e29bc45e5956c3a4e26",
                "short_code": "instr",
                "title": "Australian Nuclear Science and Technology Organisations (ANSTO) 1500L low-level radon monitor",
                "abstract": "The Australian Nuclear Science and Technology Organisations (ANSTO) 1500L low-level radon monitor provides a unique technology for highly sensitive measurements of atmospheric radon (< 100 mBq m-3) and is recognised by the World Meteorological Organisation (WMO) as the best in the world for global and atmospheric compositional baseline studies.\r\n\r\nThe ANSTO dual-flow-loop two-filter works by removing all ambient radon (222Rn) and thoron (220Rn) progeny in the sampled air from the airstream using a filter before the air passes into a large delay volume to allow for the decay of the short-lived isotope 220Rn.\r\n\r\nThe sample air in the detector is passed through a flow loop at a flow rate designed to exchange the delay volume's air in approximately 20 minutes. This allows time for new radon progeny to form. A second flow loop circulates the volume of the delay chamber through the second filter (a low-impedance 625 mesh stainless steel screen) to collect all 218Po progeny. The newly formed progeny are collected on the second filter and their decays are counted with a ZnS-photomultiplier system. Using the flow rate and the count rate the atmospheric 222Rn concentrations can be calculated.\r\n\r\nThe instrument is operated at the Weybourne Atmospheric Observatory continuously."
            },
            "relatedTo": {
                "ob_id": 30175,
                "uuid": "a957b567abf6404a81afeb13ac4bd739",
                "short_code": "acq",
                "title": "Weybourne Atmospheric Observatory: Radon concentration measurements in air from the ANSTO 1500 L detector",
                "abstract": "Weybourne Atmospheric Observatory: Radon concentration measurements in air from the ANSTO 1500 L detector"
            }
        },
        {
            "ob_id": 12314,
            "platform": {
                "ob_id": 30219,
                "uuid": "07a71f4e62e2468391f492b85905167c",
                "short_code": "plat",
                "title": "Indira Gandhi Delhi Technical University for Women (IGDTUW)",
                "abstract": "Indira Gandhi Delhi Technical University for Women (IGDTUW) which is situated on the periphery of Old Delhi and overlooks a very heavily populated area. As part of the DelhiFlux project the team have constructed a rooftop mast at 4m and a 30 m tall flux tower from which to directly measure pollutant emissions from two contrasting regions of Delhi."
            },
            "instrument": {
                "ob_id": 30218,
                "uuid": "18802d2c3e2543a2b71c90bc5ba2014b",
                "short_code": "instr",
                "title": "CEH Proton Transfer Reaction-Quadrupole ion guide Time of Flight-Mass Spectrometer (PTR-QiTOF-MS)",
                "abstract": "CEH Proton Transfer Reaction-Quadrupole ion guide Time of Flight-Mass Spectrometer (PTR-QiTOF-MS) continuously quantifies VOCs over the entire mass range in real-time delivering sub pptv-level detection limits in only a few seconds integration time."
            },
            "relatedTo": {
                "ob_id": 30220,
                "uuid": "c7579ec2abd6481d8861d416b7c6ea1c",
                "short_code": "acq",
                "title": "CEH Proton Transfer Reaction-Quadrupole ion guide Time of Flight-Mass Spectrometer (PTR-QiTOF-MS)",
                "abstract": "CEH Proton Transfer Reaction-Quadrupole ion guide Time of Flight-Mass Spectrometer (PTR-QiTOF-MS) continuously quantifies VOCs over the entire mass range in real-time delivering sub pptv-level detection limits in only a few seconds integration time."
            }
        },
        {
            "ob_id": 12315,
            "platform": {
                "ob_id": 30219,
                "uuid": "07a71f4e62e2468391f492b85905167c",
                "short_code": "plat",
                "title": "Indira Gandhi Delhi Technical University for Women (IGDTUW)",
                "abstract": "Indira Gandhi Delhi Technical University for Women (IGDTUW) which is situated on the periphery of Old Delhi and overlooks a very heavily populated area. As part of the DelhiFlux project the team have constructed a rooftop mast at 4m and a 30 m tall flux tower from which to directly measure pollutant emissions from two contrasting regions of Delhi."
            },
            "instrument": {
                "ob_id": 30218,
                "uuid": "18802d2c3e2543a2b71c90bc5ba2014b",
                "short_code": "instr",
                "title": "CEH Proton Transfer Reaction-Quadrupole ion guide Time of Flight-Mass Spectrometer (PTR-QiTOF-MS)",
                "abstract": "CEH Proton Transfer Reaction-Quadrupole ion guide Time of Flight-Mass Spectrometer (PTR-QiTOF-MS) continuously quantifies VOCs over the entire mass range in real-time delivering sub pptv-level detection limits in only a few seconds integration time."
            },
            "relatedTo": {
                "ob_id": 30222,
                "uuid": "95919182337845a7b271f66a57599779",
                "short_code": "acq",
                "title": "CEH Proton Transfer Reaction-Quadrupole ion guide Time of Flight-Mass Spectrometer (PTR-QiTOF-MS)",
                "abstract": "CEH Proton Transfer Reaction-Quadrupole ion guide Time of Flight-Mass Spectrometer (PTR-QiTOF-MS) continuously quantifies VOCs over the entire mass range in real-time delivering sub pptv-level detection limits in only a few seconds integration time."
            }
        },
        {
            "ob_id": 12316,
            "platform": {
                "ob_id": 30219,
                "uuid": "07a71f4e62e2468391f492b85905167c",
                "short_code": "plat",
                "title": "Indira Gandhi Delhi Technical University for Women (IGDTUW)",
                "abstract": "Indira Gandhi Delhi Technical University for Women (IGDTUW) which is situated on the periphery of Old Delhi and overlooks a very heavily populated area. As part of the DelhiFlux project the team have constructed a rooftop mast at 4m and a 30 m tall flux tower from which to directly measure pollutant emissions from two contrasting regions of Delhi."
            },
            "instrument": {
                "ob_id": 25495,
                "uuid": "b741b052d0bb42fb8cc70f418ac3c682",
                "short_code": "instr",
                "title": "york-gc-fid-field1",
                "abstract": "A gas chromatograph with pre-concentration unit and auto-sampler allowing for online ambient air\r\nsampling."
            },
            "relatedTo": {
                "ob_id": 30227,
                "uuid": "61176b0b41f24886b215fd48d1494416",
                "short_code": "acq",
                "title": "Acquisition for: Online measurements of VOC mixing ratios using Gas Chromatography with Flame Ionisation Detector (GC-FID) at Indira Gandhi Delhi Technical University for Women (IGDTUW)",
                "abstract": "Acquisition for: Online measurements of VOC mixing ratios using Gas Chromatography with Flame Ionisation Detector (GC-FID) at Indira Gandhi Delhi Technical University for Women (IGDTUW)"
            }
        },
        {
            "ob_id": 12317,
            "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": 25426,
                "uuid": "cfa59067ab8941b5bccb777cde14138c",
                "short_code": "instr",
                "title": "University of Lancashire/GIG: Proton Transfer Reaction-Time of Flight- Mass Spectrometer (PTR-ToF-MS)",
                "abstract": "University of Lancashire Proton Transfer Reaction-Time of Flight- Mass Spectrometer (PTR-ToF-MS) provides online measurements of volatile organic compounds in air with a high time resolution and low limit of detection. The time of flight mass analyser enables all compounds which undergo ionisation through reaction with H3O+ to be monitored simultaneously. The instrument deployed during the Atmospheric Pollution & Human Health in a Chinese Megacity programme (APHH-Beijing) field campaigns was a Ionicon PTR 2000 provided by the Guangzhou Institute of Geochemistry.\r\n \r\nThe PTR-ToF-MS is described in detail by Jordan A., Haidacher S., Hanel G., Hartungen E., Märk L., Seehauser H., Schottkowsky R., Sulzer P. and Märk T.D. (2009). A high resolution and high sensitivity proton-transfer-reaction time-of-flight mass spectrometer (PTR-TOF-MS). International Journal of Mass Spectrometry, 286, 122-128.\r\n"
            },
            "relatedTo": {
                "ob_id": 30252,
                "uuid": "c91864e40a21494886468bbc54917e53",
                "short_code": "acq",
                "title": "APHH: Volatile organic compound (VOC) flux measurements made during the APHH-Beijing field campaigns 11-12/2016 and 05-06/2017",
                "abstract": "APHH: Volatile organic compound (VOC) flux measurements made during the APHH-Beijing field campaigns 11-12/2016 and 05-06/2017"
            }
        },
        {
            "ob_id": 12318,
            "platform": {
                "ob_id": 4777,
                "uuid": "f0906665ec5e4b26bb579e5fe71a6d27",
                "short_code": "plat",
                "title": "Jersey radar station, Channel Islands",
                "abstract": "Station in the UK rain radar network, located at La Moye, Jersey, Channel Islands."
            },
            "instrument": {
                "ob_id": 13716,
                "uuid": "001ac5064d58419980facd285a6085e2",
                "short_code": "instr",
                "title": "RHUL-continuous-flow gas chromatography/isotope-ratio mass spectrometry (CF-GC/IRMS) system",
                "abstract": "The instrument is a mass spectrometer, modified for use to determine isotopic ratios of carbon12/carbon13 in either carbon dioxide (CO2) or methane (CH4). \r\n\r\nFor methane, the CO2 and carbon monoxide (CO) is removed from the sample through liquid nitrogen cryotraps and heaters. The remaining CH4 is converted to CO2 through heating and carried through to a mass spectrometer for analysis of masses 44,45 and 46, so the only remaining CO2 is from the converted CH4. \r\n\r\nSampling frequency is discrete with a precision of ~0.05 per mil. See documents for more detailed information about the instrument. "
            },
            "relatedTo": {
                "ob_id": 30268,
                "uuid": "80586d37a72044e596fc981df412d26b",
                "short_code": "acq",
                "title": "Acquisition for: d13C in CH4 regular point sampling at Jersey Radar Station, UK 2013 to 2015",
                "abstract": "Acquisition for: d13C in CH4 regular point sampling at Jersey Radar Station, UK 2013 to 2015"
            }
        },
        {
            "ob_id": 12319,
            "platform": {
                "ob_id": 30272,
                "uuid": "80ed8f5e837340a1acf127c407ace640",
                "short_code": "plat",
                "title": "Akrotiri, Cyprus",
                "abstract": "The Akrotiri Peninsula is a short peninsula which includes the southernmost point of the island of Cyprus."
            },
            "instrument": {
                "ob_id": 13716,
                "uuid": "001ac5064d58419980facd285a6085e2",
                "short_code": "instr",
                "title": "RHUL-continuous-flow gas chromatography/isotope-ratio mass spectrometry (CF-GC/IRMS) system",
                "abstract": "The instrument is a mass spectrometer, modified for use to determine isotopic ratios of carbon12/carbon13 in either carbon dioxide (CO2) or methane (CH4). \r\n\r\nFor methane, the CO2 and carbon monoxide (CO) is removed from the sample through liquid nitrogen cryotraps and heaters. The remaining CH4 is converted to CO2 through heating and carried through to a mass spectrometer for analysis of masses 44,45 and 46, so the only remaining CO2 is from the converted CH4. \r\n\r\nSampling frequency is discrete with a precision of ~0.05 per mil. See documents for more detailed information about the instrument. "
            },
            "relatedTo": {
                "ob_id": 30271,
                "uuid": "113b25e85a6d46fab50889e6225ec42a",
                "short_code": "acq",
                "title": "Acquisition for: d13C in CH4 regular point sampling and mini campaign at Akrotiri, Cyprus since 2018",
                "abstract": "Acquisition for: d13C in CH4 regular point sampling and mini campaign at Akrotiri, Cyprus since 2018"
            }
        },
        {
            "ob_id": 12320,
            "platform": {
                "ob_id": 30219,
                "uuid": "07a71f4e62e2468391f492b85905167c",
                "short_code": "plat",
                "title": "Indira Gandhi Delhi Technical University for Women (IGDTUW)",
                "abstract": "Indira Gandhi Delhi Technical University for Women (IGDTUW) which is situated on the periphery of Old Delhi and overlooks a very heavily populated area. As part of the DelhiFlux project the team have constructed a rooftop mast at 4m and a 30 m tall flux tower from which to directly measure pollutant emissions from two contrasting regions of Delhi."
            },
            "instrument": {
                "ob_id": 24965,
                "uuid": "92f530247f644823a46042777965812f",
                "short_code": "instr",
                "title": "York-Gas-AQI",
                "abstract": "Commercial gas analysers measures O3, NO, NO2, total NOy, SO2 and CO every 10 seconds. "
            },
            "relatedTo": {
                "ob_id": 30308,
                "uuid": "c04b5eef98b44f4eb8d5d64466de7429",
                "short_code": "acq",
                "title": "APHH: O3, CO, NO, NO2, NOy and SO2 measurements made at the Indira Gandhi Delhi Technical University for Women (IGDTUW) site during the pre and post monsoon periods DelhiFlux field campaign 2018",
                "abstract": "APHH: O3, CO, NO, NO2, NOy and SO2 measurements made at the Indira Gandhi Delhi Technical University for Women (IGDTUW) site during the pre and post monsoon periods DelhiFlux field campaign 2018"
            }
        },
        {
            "ob_id": 12321,
            "platform": {
                "ob_id": 30506,
                "uuid": "c58202085ddb493988be0fea4e1b065f",
                "short_code": "plat",
                "title": "Summit Station Greenland",
                "abstract": "The Summit Station in Greenland is located (72° 36’N, 38° 25’W, 3250m), atop the Greenland Ice Sheet making it a unique location for a cloud– atmosphere observatory. The station is about 400 km from the east and west coastlines and more than 1,000 km from the southwest and southeast coasts, from which most of the flow impinging on Summit originates, making it a distinctly continental environment. Additionally, the high altitude leads to extremely cold and dry conditions and a relative compression of the troposphere above the ice sheet."
            },
            "instrument": {
                "ob_id": 30504,
                "uuid": "5ff3501bc8994c8fb1d0da16f4f196d6",
                "short_code": "instr",
                "title": "ICECAPS-ACE: Condensation particle counter",
                "abstract": "The Condensation Particle Counter (CPC) is a GRIMM CPC 5.400. The CPC is located on the roof of the MSF building at Summit station, 72.578590N -38.452693E, approximately 3 m from the ground (depending on snow drifting/ accumulation).  Inlet losses are < 15% for particle sizes 0.08 to 1 μm diameter. Inlet losses are > 50 % for particles smaller than 0.02 μm and larger than 2.2 μm diameter. \r\n\r\nThese data were collected as part of the joint Natural Environmental Research Council (NERC) and US National Science Foundation (NSF) -funded Integrated Characterisation of Energy, Clouds, Atmospheric state, and Precipitation at Summit - Aerosol Cloud Experiment (ICECAPS-ACE) project."
            },
            "relatedTo": {
                "ob_id": 30503,
                "uuid": "4543cd6035994c8993f46c875c88628b",
                "short_code": "acq",
                "title": "Acquisition for: Summit Aerosol Cloud Experiment: surface aerosol concentration (condensation nuclei > 5nm diameter)",
                "abstract": "Acquisition for: Summit Aerosol Cloud Experiment: surface aerosol concentration (condensation nuclei > 5nm diameter)"
            }
        },
        {
            "ob_id": 12322,
            "platform": {
                "ob_id": 30506,
                "uuid": "c58202085ddb493988be0fea4e1b065f",
                "short_code": "plat",
                "title": "Summit Station Greenland",
                "abstract": "The Summit Station in Greenland is located (72° 36’N, 38° 25’W, 3250m), atop the Greenland Ice Sheet making it a unique location for a cloud– atmosphere observatory. The station is about 400 km from the east and west coastlines and more than 1,000 km from the southwest and southeast coasts, from which most of the flow impinging on Summit originates, making it a distinctly continental environment. Additionally, the high altitude leads to extremely cold and dry conditions and a relative compression of the troposphere above the ice sheet."
            },
            "instrument": {
                "ob_id": 30510,
                "uuid": "376bd8a114e34dc1b97e2e698c555096",
                "short_code": "instr",
                "title": "ICECAPS-ACE: SKYOPC optical particle counter",
                "abstract": "The GRIMM SKYOPC 1.129 Optical particle counter is located on the roof of the MSF building at Summit station, 72.578590N -38.452693E. Approximately 3 m from the ground (depending on snow drifting/ accumulation). The instrument measures surface aerosol size distribution (0.25 to 6.5 um diameter).\r\nData are corrected for particle loss in the inlet.\r\n\r\nThese data were collected as part of the joint Natural Environmental Research Council (NERC) and US National Science Foundation (NSF) -funded Integrated Characterisation of Energy, Clouds, Atmospheric state, and Precipitation at Summit - Aerosol Cloud Experiment (ICECAPS-ACE) project."
            },
            "relatedTo": {
                "ob_id": 30511,
                "uuid": "0f328ee20e7d47c4bfd443a34a2be3a3",
                "short_code": "acq",
                "title": "ICECAPS-ACE: Summit Aerosol Cloud Experiment: surface aerosol size distribution (0.25 to 6.5 um diameter) taken at Summit Station Greenland",
                "abstract": "ICECAPS-ACE: Summit Aerosol Cloud Experiment: surface aerosol size distribution (0.25 to 6.5 um diameter) taken at Summit Station Greenland"
            }
        },
        {
            "ob_id": 12323,
            "platform": {
                "ob_id": 30506,
                "uuid": "c58202085ddb493988be0fea4e1b065f",
                "short_code": "plat",
                "title": "Summit Station Greenland",
                "abstract": "The Summit Station in Greenland is located (72° 36’N, 38° 25’W, 3250m), atop the Greenland Ice Sheet making it a unique location for a cloud– atmosphere observatory. The station is about 400 km from the east and west coastlines and more than 1,000 km from the southwest and southeast coasts, from which most of the flow impinging on Summit originates, making it a distinctly continental environment. Additionally, the high altitude leads to extremely cold and dry conditions and a relative compression of the troposphere above the ice sheet."
            },
            "instrument": {
                "ob_id": 30514,
                "uuid": "0c930a24be924ece9e4c123c81a85e42",
                "short_code": "instr",
                "title": "ICECAPS-ACE: KT15 Infrared Temperature sensor",
                "abstract": "Heitronics KT15 IR temperature sensor (number 1) is a digital, compact, programmable and universally applicable radiation pyrometer series with comprehensive and flexible functions for industrial temperature monitoring and control. It measures surface temperature remotely from infrared radiation.\r\n\r\nThe KT15.85 IIP model is able to measure between -25 and 200 °C.\r\n\r\nData are measured and outputted at 1Hz.\r\n\r\nIt features:\r\n- Extreme high stability due to Chopped Radiation Method\r\n- Very high resolution 0.03 °C\r\n- Fast response times from 5 ms on low temperatures\r\n- Very high linearization accuracy (0.02K)\r\n- Fields-of-view from 0.7 mm at low temperatures allow high optical resolutions\r\n- Permanent self-monitoring routines ensure a reliable operation\r\n- Integrated calibration routine allows for fast and reliable control of the device.\r\n\r\nThese data were collected as part of the joint Natural Environmental Research Council (NERC) and US National Science Foundation (NSF) -funded Integrated Characterisation of Energy, Clouds, Atmospheric state, and Precipitation at Summit - Aerosol Cloud Experiment (ICECAPS-ACE) project."
            },
            "relatedTo": {
                "ob_id": 30515,
                "uuid": "36541e8eaa5e4cffa6620eca333485a8",
                "short_code": "acq",
                "title": "ICECAPS-ACE: Summit Aerosol Cloud Experiment: surface snow surface brightness temperature taken at Summit Station Greenland",
                "abstract": "ICECAPS-ACE: Summit Aerosol Cloud Experiment: surface snow surface brightness temperature taken at Summit Station Greenland"
            }
        },
        {
            "ob_id": 12324,
            "platform": {
                "ob_id": 30506,
                "uuid": "c58202085ddb493988be0fea4e1b065f",
                "short_code": "plat",
                "title": "Summit Station Greenland",
                "abstract": "The Summit Station in Greenland is located (72° 36’N, 38° 25’W, 3250m), atop the Greenland Ice Sheet making it a unique location for a cloud– atmosphere observatory. The station is about 400 km from the east and west coastlines and more than 1,000 km from the southwest and southeast coasts, from which most of the flow impinging on Summit originates, making it a distinctly continental environment. Additionally, the high altitude leads to extremely cold and dry conditions and a relative compression of the troposphere above the ice sheet."
            },
            "instrument": {
                "ob_id": 30517,
                "uuid": "ad664313257843ef820f5f9a6671eac1",
                "short_code": "instr",
                "title": "ICECAPS-ACE: temperature and humidity sensors",
                "abstract": "Four Vaisala HMP155 T/RH sensors with heated probe. Each sensor is mounted on the Met tower at Summit station inside an aspirated shield. \r\n\r\nTower location: -38.470361E, 72.572962N\r\nTower top elevation: 3267 masl\r\nHMP1 elevation: Tower top - 12.3 m \r\nHMP2 elevation: Tower top - 9.8 m \r\nHMP3 elevation: Tower top - 4.5 m \r\nHMP4 elevation: Tower top - 1.0 m\r\n\r\nThese data were collected as part of the joint Natural Environmental Research Council (NERC) and US National Science Foundation (NSF) -funded Integrated Characterisation of Energy, Clouds, Atmospheric state, and Precipitation at Summit - Aerosol Cloud Experiment (ICECAPS-ACE) project."
            },
            "relatedTo": {
                "ob_id": 30518,
                "uuid": "b93898380bd74bb5831980b4e231894c",
                "short_code": "acq",
                "title": "ICECAPS-ACE: Summit Aerosol Cloud Experiment: surface moisture profile taken at Summit Station Greenland",
                "abstract": "ICECAPS-ACE: Summit Aerosol Cloud Experiment: surface moisture profile taken at Summit Station Greenland"
            }
        },
        {
            "ob_id": 12325,
            "platform": {
                "ob_id": 30506,
                "uuid": "c58202085ddb493988be0fea4e1b065f",
                "short_code": "plat",
                "title": "Summit Station Greenland",
                "abstract": "The Summit Station in Greenland is located (72° 36’N, 38° 25’W, 3250m), atop the Greenland Ice Sheet making it a unique location for a cloud– atmosphere observatory. The station is about 400 km from the east and west coastlines and more than 1,000 km from the southwest and southeast coasts, from which most of the flow impinging on Summit originates, making it a distinctly continental environment. Additionally, the high altitude leads to extremely cold and dry conditions and a relative compression of the troposphere above the ice sheet."
            },
            "instrument": {
                "ob_id": 30521,
                "uuid": "cc11cd5f3d86477cb19542e8724fd443",
                "short_code": "instr",
                "title": "ICECAPS-ACE: Sonic distance sensor",
                "abstract": "The SR50AH Heated Sonic Distance Sensor provides a non-contact method for determining snow depth. It determines depth by emitting an ultrasonic pulse and then measuring the elapsed time between the emission and return of the pulse. An air temperature measurement is required to correct for variations of the speed of sound in air. The SR50AH includes an integrated heater that prevents ice and rime from coating the transducer.\r\n\r\nThese data were collected as part of the joint Natural Environmental Research Council (NERC) and US National Science Foundation (NSF) -funded Integrated Characterisation of Energy, Clouds, Atmospheric state, and Precipitation at Summit - Aerosol Cloud Experiment (ICECAPS-ACE) project."
            },
            "relatedTo": {
                "ob_id": 30522,
                "uuid": "d0c0e525a3a0415d92007e50d8191154",
                "short_code": "acq",
                "title": "ICECAPS-ACE: Summit Aerosol Cloud Experiment: snow height change taken at Summit Station Greenland",
                "abstract": "ICECAPS-ACE: Summit Aerosol Cloud Experiment: snow height change taken at Summit Station Greenland"
            }
        },
        {
            "ob_id": 12326,
            "platform": {
                "ob_id": 30506,
                "uuid": "c58202085ddb493988be0fea4e1b065f",
                "short_code": "plat",
                "title": "Summit Station Greenland",
                "abstract": "The Summit Station in Greenland is located (72° 36’N, 38° 25’W, 3250m), atop the Greenland Ice Sheet making it a unique location for a cloud– atmosphere observatory. The station is about 400 km from the east and west coastlines and more than 1,000 km from the southwest and southeast coasts, from which most of the flow impinging on Summit originates, making it a distinctly continental environment. Additionally, the high altitude leads to extremely cold and dry conditions and a relative compression of the troposphere above the ice sheet."
            },
            "instrument": {
                "ob_id": 30527,
                "uuid": "564902c867344874990aa33a807d3ab1",
                "short_code": "instr",
                "title": "ICECAPS-ACE: heated anemometer",
                "abstract": "Surface wind profiles measured using the following anemometers:\r\n\r\nLufft VentusX, heated 2D sonic anemometer. \r\nMetek uSonic-3 Scientific, heated 3D sonic anemometer. \r\n\r\nEach sensor is mounted on the Met tower at Summit station.\r\n\r\nThese data were collected as part of the joint Natural Environmental Research Council (NERC) and US National Science Foundation (NSF) -funded Integrated Characterisation of Energy, Clouds, Atmospheric state, and Precipitation at Summit - Aerosol Cloud Experiment (ICECAPS-ACE) project."
            },
            "relatedTo": {
                "ob_id": 30528,
                "uuid": "c96183e0c2404079bea95db62d9e00b5",
                "short_code": "acq",
                "title": "ICECAPS-ACE: Summit Aerosol Cloud Experiment: surface wind profiles taken at Summit Station Greenland",
                "abstract": "ICECAPS-ACE: Summit Aerosol Cloud Experiment: surface wind profiles taken at Summit Station Greenland"
            }
        },
        {
            "ob_id": 12327,
            "platform": {
                "ob_id": 30539,
                "uuid": "1731a99804b84284910aa3ddf9522360",
                "short_code": "plat",
                "title": "Llanos de Moxos wetland",
                "abstract": "Llanos de Moxos wetland is located near Trinidad, Bolivia."
            },
            "instrument": {
                "ob_id": 13716,
                "uuid": "001ac5064d58419980facd285a6085e2",
                "short_code": "instr",
                "title": "RHUL-continuous-flow gas chromatography/isotope-ratio mass spectrometry (CF-GC/IRMS) system",
                "abstract": "The instrument is a mass spectrometer, modified for use to determine isotopic ratios of carbon12/carbon13 in either carbon dioxide (CO2) or methane (CH4). \r\n\r\nFor methane, the CO2 and carbon monoxide (CO) is removed from the sample through liquid nitrogen cryotraps and heaters. The remaining CH4 is converted to CO2 through heating and carried through to a mass spectrometer for analysis of masses 44,45 and 46, so the only remaining CO2 is from the converted CH4. \r\n\r\nSampling frequency is discrete with a precision of ~0.05 per mil. See documents for more detailed information about the instrument. "
            },
            "relatedTo": {
                "ob_id": 30538,
                "uuid": "35b3c376dd124115aac4aa2495fb928d",
                "short_code": "acq",
                "title": "Acquisition for:  Methane Observations and Yearly Assessments (MOYA): Isotopic d13C methane measurements taken from Llanos de Moxos, Bolivia 2019",
                "abstract": "Acquisition for:  Methane Observations and Yearly Assessments (MOYA): Isotopic d13C methane measurements taken from Llanos de Moxos, Bolivia 2019"
            }
        },
        {
            "ob_id": 12328,
            "platform": {
                "ob_id": 30547,
                "uuid": "5a024bc936834528bf30efec8364c379",
                "short_code": "plat",
                "title": "Cape Point",
                "abstract": "Cape Point is a promontory at the southeast corner of the Cape Peninsula, which is a mountainous and scenic landform that runs north-south for about thirty kilometres at the extreme southwestern tip of the African continent in the Republic of South Africa. Table Mountain and the city of Cape Town are close to the northern extremity of the same peninsula. The cape is located at 34°21′26″S 18°29′51″ECoordinates: 34°21′26″S 18°29′51″E, about 2.3 kilometres (1.4 mi) east and a little north of the Cape of Good Hope on the southwest corner"
            },
            "instrument": {
                "ob_id": 13716,
                "uuid": "001ac5064d58419980facd285a6085e2",
                "short_code": "instr",
                "title": "RHUL-continuous-flow gas chromatography/isotope-ratio mass spectrometry (CF-GC/IRMS) system",
                "abstract": "The instrument is a mass spectrometer, modified for use to determine isotopic ratios of carbon12/carbon13 in either carbon dioxide (CO2) or methane (CH4). \r\n\r\nFor methane, the CO2 and carbon monoxide (CO) is removed from the sample through liquid nitrogen cryotraps and heaters. The remaining CH4 is converted to CO2 through heating and carried through to a mass spectrometer for analysis of masses 44,45 and 46, so the only remaining CO2 is from the converted CH4. \r\n\r\nSampling frequency is discrete with a precision of ~0.05 per mil. See documents for more detailed information about the instrument. "
            },
            "relatedTo": {
                "ob_id": 30546,
                "uuid": "7ef6978f0617472c80bd35f168af6296",
                "short_code": "acq",
                "title": "Acquisition for: Methane Observations and Yearly Assessments (MOYA): Isotopic d13C methane measurements taken from Cape Point Observatory Station, South Africa 2011 to 2016",
                "abstract": "Acquisition for: Methane Observations and Yearly Assessments (MOYA): Isotopic d13C methane measurements taken from Cape Point Observatory Station, South Africa 2011 to 2016"
            }
        },
        {
            "ob_id": 12329,
            "platform": {
                "ob_id": 30551,
                "uuid": "c10b0555c93d414e95a3714180ef23eb",
                "short_code": "plat",
                "title": "Royal Holloway Earth Sciences Monitoring Station",
                "abstract": "Royal Holloway Earth Sciences Monitoring Station"
            },
            "instrument": {
                "ob_id": 13716,
                "uuid": "001ac5064d58419980facd285a6085e2",
                "short_code": "instr",
                "title": "RHUL-continuous-flow gas chromatography/isotope-ratio mass spectrometry (CF-GC/IRMS) system",
                "abstract": "The instrument is a mass spectrometer, modified for use to determine isotopic ratios of carbon12/carbon13 in either carbon dioxide (CO2) or methane (CH4). \r\n\r\nFor methane, the CO2 and carbon monoxide (CO) is removed from the sample through liquid nitrogen cryotraps and heaters. The remaining CH4 is converted to CO2 through heating and carried through to a mass spectrometer for analysis of masses 44,45 and 46, so the only remaining CO2 is from the converted CH4. \r\n\r\nSampling frequency is discrete with a precision of ~0.05 per mil. See documents for more detailed information about the instrument. "
            },
            "relatedTo": {
                "ob_id": 30550,
                "uuid": "e238399044e14ab487aa5f2abfc2e048",
                "short_code": "acq",
                "title": "Acquisition for: Methane Observations and Yearly Assessments (MOYA): Isotopic d13C methane measurements taken from Royal Holloway Earth Sciences Monitoring Station, Egham, UK, 2015 to 2020",
                "abstract": "Acquisition for: Methane Observations and Yearly Assessments (MOYA): Isotopic d13C methane measurements taken from Royal Holloway Earth Sciences Monitoring Station, Egham, UK, 2015 to 2020"
            }
        },
        {
            "ob_id": 12330,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V &#8211; 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 30558,
                "uuid": "1c3aa52da4ef43fa837d684930569089",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20200608133202__ ARSF 2014_309 - MA14_14 Flight: data acquisition details",
                "abstract": "ARSF 2014_309 - MA14_14 Flight data acquisition details."
            }
        },
        {
            "ob_id": 12331,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V &#8211; 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": 30558,
                "uuid": "1c3aa52da4ef43fa837d684930569089",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20200608133202__ ARSF 2014_309 - MA14_14 Flight: data acquisition details",
                "abstract": "ARSF 2014_309 - MA14_14 Flight data acquisition details."
            }
        },
        {
            "ob_id": 12332,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V &#8211; 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 30558,
                "uuid": "1c3aa52da4ef43fa837d684930569089",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20200608133202__ ARSF 2014_309 - MA14_14 Flight: data acquisition details",
                "abstract": "ARSF 2014_309 - MA14_14 Flight data acquisition details."
            }
        },
        {
            "ob_id": 12333,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V &#8211; 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 30559,
                "uuid": "d02d0cecbc3d44e298371b5cd4124413",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20200608133204__ ARSF 2014_309 - MA14_14 Flight: data acquisition details",
                "abstract": "ARSF 2014_309 - MA14_14 Flight data acquisition details."
            }
        },
        {
            "ob_id": 12334,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V &#8211; 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": 30559,
                "uuid": "d02d0cecbc3d44e298371b5cd4124413",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20200608133204__ ARSF 2014_309 - MA14_14 Flight: data acquisition details",
                "abstract": "ARSF 2014_309 - MA14_14 Flight data acquisition details."
            }
        },
        {
            "ob_id": 12335,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V &#8211; 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 30559,
                "uuid": "d02d0cecbc3d44e298371b5cd4124413",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20200608133204__ ARSF 2014_309 - MA14_14 Flight: data acquisition details",
                "abstract": "ARSF 2014_309 - MA14_14 Flight data acquisition details."
            }
        },
        {
            "ob_id": 12336,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V &#8211; 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24847,
                "uuid": "4557fda0ad78453ca5658354289e1370",
                "short_code": "instr",
                "title": "NERC-ARF Leica RCD105",
                "abstract": "The Leica RCD105 medium format digital camera produces 16 bit TIFF digital images at 7216x5412 resolution (39 Mega-pixels)."
            },
            "relatedTo": {
                "ob_id": 30560,
                "uuid": "2dd6d4e99595497ab78187b681604d81",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20200608133211__ ARSF 2014_309 - MA14_14 Flight: data acquisition details",
                "abstract": "ARSF 2014_309 - MA14_14 Flight data acquisition details."
            }
        },
        {
            "ob_id": 12337,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V &#8211; 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": 30560,
                "uuid": "2dd6d4e99595497ab78187b681604d81",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20200608133211__ ARSF 2014_309 - MA14_14 Flight: data acquisition details",
                "abstract": "ARSF 2014_309 - MA14_14 Flight data acquisition details."
            }
        },
        {
            "ob_id": 12338,
            "platform": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V &#8211; 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "instrument": {
                "ob_id": 24846,
                "uuid": "d5f3a581307b406cae4ff20bc0af1f85",
                "short_code": "instr",
                "title": "NERC-ARF Leica ALS50-II LiDAR",
                "abstract": "The Leica ALS50-II LiDAR is a Light Detection and Ranging instrument flown on the NERC-ARF aircraft capable of producing both discrete point clouds and full-waveform returns. With a laser of wavelength 1064 nm pulsed at 4 ns or 9 ns it is suitable for high accuracy topographic applications. The data can be used to create Digital Elevation Models or represent 3D structures such as tree canopies."
            },
            "relatedTo": {
                "ob_id": 30560,
                "uuid": "2dd6d4e99595497ab78187b681604d81",
                "short_code": "acq",
                "title": "__MUST_UPDATE__20200608133211__ ARSF 2014_309 - MA14_14 Flight: data acquisition details",
                "abstract": "ARSF 2014_309 - MA14_14 Flight data acquisition details."
            }
        }
    ]
}