Procedure Acquisition List

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{
    "count": 5833,
    "next": "https://api.catalogue.ceda.ac.uk/api/v3/acquisitions/?format=api&limit=100&offset=2500",
    "previous": "https://api.catalogue.ceda.ac.uk/api/v3/acquisitions/?format=api&limit=100&offset=2300",
    "results": [
        {
            "ob_id": 10768,
            "uuid": "50864d02527a4f7ebeac3c328a4b26e7",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Optech LIDAR Instrument on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB06/05 over the Clocaenog Forest and Glasfyndd Forest Areas",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3776,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8621,
                        "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                        "short_code": "instr",
                        "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                        "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
                    },
                    "relatedTo": {
                        "ob_id": 10768,
                        "uuid": "50864d02527a4f7ebeac3c328a4b26e7",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Optech LIDAR Instrument on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB06/05 over the Clocaenog Forest and Glasfyndd Forest Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10772,
            "uuid": "34f165786ab4493497974fb30098a53b",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/13 over the Skeidararjokull Area, Iceland",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3777,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8621,
                        "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                        "short_code": "instr",
                        "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                        "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
                    },
                    "relatedTo": {
                        "ob_id": 10772,
                        "uuid": "34f165786ab4493497974fb30098a53b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/13 over the Skeidararjokull Area, Iceland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3778,
                    "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": 10772,
                        "uuid": "34f165786ab4493497974fb30098a53b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/13 over the Skeidararjokull Area, Iceland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3779,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10772,
                        "uuid": "34f165786ab4493497974fb30098a53b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/13 over the Skeidararjokull Area, Iceland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3780,
                    "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": 10772,
                        "uuid": "34f165786ab4493497974fb30098a53b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/13 over the Skeidararjokull Area, Iceland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10776,
            "uuid": "aacdb2d7c376450abcb8e1054edf343e",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/10 over the Russel Glacier, Greenland",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3781,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10776,
                        "uuid": "aacdb2d7c376450abcb8e1054edf343e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/10 over the Russel Glacier, Greenland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3782,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8626,
                        "uuid": "c069d0c60e0345b8b37d1c28adfb4db9",
                        "short_code": "instr",
                        "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)",
                        "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present"
                    },
                    "relatedTo": {
                        "ob_id": 10776,
                        "uuid": "aacdb2d7c376450abcb8e1054edf343e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/10 over the Russel Glacier, Greenland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3783,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8621,
                        "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                        "short_code": "instr",
                        "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                        "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
                    },
                    "relatedTo": {
                        "ob_id": 10776,
                        "uuid": "aacdb2d7c376450abcb8e1054edf343e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/10 over the Russel Glacier, Greenland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3784,
                    "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": 10776,
                        "uuid": "aacdb2d7c376450abcb8e1054edf343e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/10 over the Russel Glacier, Greenland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3785,
                    "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": 10776,
                        "uuid": "aacdb2d7c376450abcb8e1054edf343e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/10 over the Russel Glacier, Greenland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10780,
            "uuid": "833713a1159c47eaa42cd310fab85ec4",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/05 over the Mojo Area, Ethiopia",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3786,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8621,
                        "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                        "short_code": "instr",
                        "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                        "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
                    },
                    "relatedTo": {
                        "ob_id": 10780,
                        "uuid": "833713a1159c47eaa42cd310fab85ec4",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/05 over the Mojo Area, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3787,
                    "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": 10780,
                        "uuid": "833713a1159c47eaa42cd310fab85ec4",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/05 over the Mojo Area, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3788,
                    "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": 10780,
                        "uuid": "833713a1159c47eaa42cd310fab85ec4",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/05 over the Mojo Area, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3789,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10780,
                        "uuid": "833713a1159c47eaa42cd310fab85ec4",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/05 over the Mojo Area, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10784,
            "uuid": "837e5ad985a74efa8e68529c49788fa3",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/09 over the Krafla Area, Iceland",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Specim AISA Eagle, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3790,
                    "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": 10784,
                        "uuid": "837e5ad985a74efa8e68529c49788fa3",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/09 over the Krafla Area, Iceland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Specim AISA Eagle, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3791,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10784,
                        "uuid": "837e5ad985a74efa8e68529c49788fa3",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/09 over the Krafla Area, Iceland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Specim AISA Eagle, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3792,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8626,
                        "uuid": "c069d0c60e0345b8b37d1c28adfb4db9",
                        "short_code": "instr",
                        "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)",
                        "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present"
                    },
                    "relatedTo": {
                        "ob_id": 10784,
                        "uuid": "837e5ad985a74efa8e68529c49788fa3",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/09 over the Krafla Area, Iceland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Specim AISA Eagle, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3793,
                    "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": 10784,
                        "uuid": "837e5ad985a74efa8e68529c49788fa3",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/09 over the Krafla Area, Iceland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Specim AISA Eagle, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3794,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 7858,
                        "uuid": "ee7d3a6b6a1e4101b58538749b075030",
                        "short_code": "instr",
                        "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)",
                        "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres."
                    },
                    "relatedTo": {
                        "ob_id": 10784,
                        "uuid": "837e5ad985a74efa8e68529c49788fa3",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/09 over the Krafla Area, Iceland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Specim AISA Eagle, ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10788,
            "uuid": "5bfdeecd3b25446daf6cefde87647119",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/06 over the Konso Area, Ethiopia",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Specim AISA Hawk, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Eagle, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3795,
                    "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": 10788,
                        "uuid": "5bfdeecd3b25446daf6cefde87647119",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/06 over the Konso Area, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Specim AISA Hawk, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Eagle, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3796,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8621,
                        "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                        "short_code": "instr",
                        "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                        "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
                    },
                    "relatedTo": {
                        "ob_id": 10788,
                        "uuid": "5bfdeecd3b25446daf6cefde87647119",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/06 over the Konso Area, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Specim AISA Hawk, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Eagle, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3797,
                    "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": 10788,
                        "uuid": "5bfdeecd3b25446daf6cefde87647119",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/06 over the Konso Area, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Specim AISA Hawk, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Eagle, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3798,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10788,
                        "uuid": "5bfdeecd3b25446daf6cefde87647119",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/06 over the Konso Area, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Specim AISA Hawk, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Eagle, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10792,
            "uuid": "b139169f1ed64bf5997451e8905f6cda",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 90/44 over the Somerset Lakes - Chilton Trinity, Blagdon, Chew Valley, Emborough and Shearwater",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8692,
                    "uuid": "f6f35b2e9a39416c987e8ff7eca15995",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft",
                    "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3799,
                    "platform": {
                        "ob_id": 8691,
                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
                        "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983."
                    },
                    "instrument": {
                        "ob_id": 8855,
                        "uuid": "675df2bd79404c8ba30c6991111df9e7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC8 Analogue Photographic camera",
                        "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n"
                    },
                    "relatedTo": {
                        "ob_id": 10792,
                        "uuid": "b139169f1ed64bf5997451e8905f6cda",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 90/44 over the Somerset Lakes - Chilton Trinity, Blagdon, Chew Valley, Emborough and Shearwater",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 10796,
            "uuid": "2b7dba2645104df5807190949aeb9b26",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 Aircraft during Flight GB08/02 over the Delamere Wood Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3800,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8626,
                        "uuid": "c069d0c60e0345b8b37d1c28adfb4db9",
                        "short_code": "instr",
                        "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)",
                        "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present"
                    },
                    "relatedTo": {
                        "ob_id": 10796,
                        "uuid": "2b7dba2645104df5807190949aeb9b26",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 Aircraft during Flight GB08/02 over the Delamere Wood Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3801,
                    "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": 10796,
                        "uuid": "2b7dba2645104df5807190949aeb9b26",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 Aircraft during Flight GB08/02 over the Delamere Wood Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3802,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10796,
                        "uuid": "2b7dba2645104df5807190949aeb9b26",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 Aircraft during Flight GB08/02 over the Delamere Wood Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3803,
                    "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": 10796,
                        "uuid": "2b7dba2645104df5807190949aeb9b26",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 Aircraft during Flight GB08/02 over the Delamere Wood Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Specim AISA Hawk, ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10800,
            "uuid": "af1a1afc8b564a78ad4fcff8f01b0783",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the CASI and ATM Instruments on-board the Piper PA31 Navajo Chieftain Aircraft during Flight 95/13 over the Guadalfeo River Basin, Spain",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 1 (CASI-1), ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8692,
                    "uuid": "f6f35b2e9a39416c987e8ff7eca15995",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft",
                    "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3804,
                    "platform": {
                        "ob_id": 8691,
                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
                        "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983."
                    },
                    "instrument": {
                        "ob_id": 8701,
                        "uuid": "0207b70a7b5543de832f5a0d49320cbe",
                        "short_code": "instr",
                        "title": "ARSF Compact Airbone Spectrographic Imager 1 (CASI-1)",
                        "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 1"
                    },
                    "relatedTo": {
                        "ob_id": 10800,
                        "uuid": "af1a1afc8b564a78ad4fcff8f01b0783",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the CASI and ATM Instruments on-board the Piper PA31 Navajo Chieftain Aircraft during Flight 95/13 over the Guadalfeo River Basin, Spain",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 1 (CASI-1), ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                },
                {
                    "ob_id": 3805,
                    "platform": {
                        "ob_id": 8691,
                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
                        "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983."
                    },
                    "instrument": {
                        "ob_id": 8754,
                        "uuid": "967ae4b17bf145d8a8a6982a648d64d5",
                        "short_code": "instr",
                        "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268",
                        "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998."
                    },
                    "relatedTo": {
                        "ob_id": 10800,
                        "uuid": "af1a1afc8b564a78ad4fcff8f01b0783",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the CASI and ATM Instruments on-board the Piper PA31 Navajo Chieftain Aircraft during Flight 95/13 over the Guadalfeo River Basin, Spain",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 1 (CASI-1), ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 10804,
            "uuid": "c2c4f241b45d44b2a782d1d9c2aa1481",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain Aircraft during Flight 99/10 over the Petersfield and Thorney Island Areas",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 1 (CASI-1), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8692,
                    "uuid": "f6f35b2e9a39416c987e8ff7eca15995",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft",
                    "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3806,
                    "platform": {
                        "ob_id": 8691,
                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
                        "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983."
                    },
                    "instrument": {
                        "ob_id": 8701,
                        "uuid": "0207b70a7b5543de832f5a0d49320cbe",
                        "short_code": "instr",
                        "title": "ARSF Compact Airbone Spectrographic Imager 1 (CASI-1)",
                        "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 1"
                    },
                    "relatedTo": {
                        "ob_id": 10804,
                        "uuid": "c2c4f241b45d44b2a782d1d9c2aa1481",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain Aircraft during Flight 99/10 over the Petersfield and Thorney Island Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 1 (CASI-1), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                },
                {
                    "ob_id": 3807,
                    "platform": {
                        "ob_id": 8691,
                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
                        "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983."
                    },
                    "instrument": {
                        "ob_id": 8626,
                        "uuid": "c069d0c60e0345b8b37d1c28adfb4db9",
                        "short_code": "instr",
                        "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)",
                        "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present"
                    },
                    "relatedTo": {
                        "ob_id": 10804,
                        "uuid": "c2c4f241b45d44b2a782d1d9c2aa1481",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain Aircraft during Flight 99/10 over the Petersfield and Thorney Island Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 1 (CASI-1), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 10808,
            "uuid": "6e66c3c136924b7997685d2a53601ed8",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the CASI-2 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/06 over the Dorchester and New Forest Areas, to Validate Envisat MERIS Terrestrial Chlorophyll Index (MTCI) Data",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3808,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 7858,
                        "uuid": "ee7d3a6b6a1e4101b58538749b075030",
                        "short_code": "instr",
                        "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)",
                        "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres."
                    },
                    "relatedTo": {
                        "ob_id": 10808,
                        "uuid": "6e66c3c136924b7997685d2a53601ed8",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the CASI-2 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/06 over the Dorchester and New Forest Areas, to Validate Envisat MERIS Terrestrial Chlorophyll Index (MTCI) Data",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3809,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8621,
                        "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                        "short_code": "instr",
                        "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                        "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
                    },
                    "relatedTo": {
                        "ob_id": 10808,
                        "uuid": "6e66c3c136924b7997685d2a53601ed8",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the CASI-2 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/06 over the Dorchester and New Forest Areas, to Validate Envisat MERIS Terrestrial Chlorophyll Index (MTCI) Data",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10812,
            "uuid": "a1c58a5cacf54183a51e656024900c8a",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB08/19 over the London Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3810,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10812,
                        "uuid": "a1c58a5cacf54183a51e656024900c8a",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB08/19 over the London Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3811,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8626,
                        "uuid": "c069d0c60e0345b8b37d1c28adfb4db9",
                        "short_code": "instr",
                        "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)",
                        "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present"
                    },
                    "relatedTo": {
                        "ob_id": 10812,
                        "uuid": "a1c58a5cacf54183a51e656024900c8a",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB08/19 over the London Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3812,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8621,
                        "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                        "short_code": "instr",
                        "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                        "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
                    },
                    "relatedTo": {
                        "ob_id": 10812,
                        "uuid": "a1c58a5cacf54183a51e656024900c8a",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB08/19 over the London Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3813,
                    "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": 10812,
                        "uuid": "a1c58a5cacf54183a51e656024900c8a",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB08/19 over the London Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3814,
                    "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": 10812,
                        "uuid": "a1c58a5cacf54183a51e656024900c8a",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB08/19 over the London Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10816,
            "uuid": "0b5a57b7a1eb454c90c2d8832b60bdc2",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 86/49 over the River Taff",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8692,
                    "uuid": "f6f35b2e9a39416c987e8ff7eca15995",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft",
                    "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3815,
                    "platform": {
                        "ob_id": 8691,
                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
                        "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983."
                    },
                    "instrument": {
                        "ob_id": 8855,
                        "uuid": "675df2bd79404c8ba30c6991111df9e7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC8 Analogue Photographic camera",
                        "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n"
                    },
                    "relatedTo": {
                        "ob_id": 10816,
                        "uuid": "0b5a57b7a1eb454c90c2d8832b60bdc2",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 86/49 over the River Taff",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 10820,
            "uuid": "9a743adb99e84a4eb2430e4273256cdb",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/05 over the Loch Leven, Windermere and Esthwaite Water Areas",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3816,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8626,
                        "uuid": "c069d0c60e0345b8b37d1c28adfb4db9",
                        "short_code": "instr",
                        "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)",
                        "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present"
                    },
                    "relatedTo": {
                        "ob_id": 10820,
                        "uuid": "9a743adb99e84a4eb2430e4273256cdb",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/05 over the Loch Leven, Windermere and Esthwaite Water Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3817,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 7858,
                        "uuid": "ee7d3a6b6a1e4101b58538749b075030",
                        "short_code": "instr",
                        "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)",
                        "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres."
                    },
                    "relatedTo": {
                        "ob_id": 10820,
                        "uuid": "9a743adb99e84a4eb2430e4273256cdb",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/05 over the Loch Leven, Windermere and Esthwaite Water Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3818,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10820,
                        "uuid": "9a743adb99e84a4eb2430e4273256cdb",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/05 over the Loch Leven, Windermere and Esthwaite Water Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3819,
                    "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": 10820,
                        "uuid": "9a743adb99e84a4eb2430e4273256cdb",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/05 over the Loch Leven, Windermere and Esthwaite Water Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3820,
                    "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": 10820,
                        "uuid": "9a743adb99e84a4eb2430e4273256cdb",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2, ATM AZ-16 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/05 over the Loch Leven, Windermere and Esthwaite Water Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10824,
            "uuid": "aaefe4d931e54b018e76d32137239c80",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/03 over the Sandflug Area, Greenland",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3821,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8621,
                        "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                        "short_code": "instr",
                        "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                        "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
                    },
                    "relatedTo": {
                        "ob_id": 10824,
                        "uuid": "aaefe4d931e54b018e76d32137239c80",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/03 over the Sandflug Area, Greenland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3822,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8626,
                        "uuid": "c069d0c60e0345b8b37d1c28adfb4db9",
                        "short_code": "instr",
                        "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)",
                        "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present"
                    },
                    "relatedTo": {
                        "ob_id": 10824,
                        "uuid": "aaefe4d931e54b018e76d32137239c80",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/03 over the Sandflug Area, Greenland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3823,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10824,
                        "uuid": "aaefe4d931e54b018e76d32137239c80",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, ATM AZ-16 and Optech LIDAR Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight IPY07/03 over the Sandflug Area, Greenland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10828,
            "uuid": "73d76f0f466f4250a8c6910a53b2d416",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/02 over the Difarsa Area, Nile Gorge, Ethiopia",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3824,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10828,
                        "uuid": "73d76f0f466f4250a8c6910a53b2d416",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/02 over the Difarsa Area, Nile Gorge, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3825,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8621,
                        "uuid": "29e351cfcf014044af5f9f1e3d3678d0",
                        "short_code": "instr",
                        "title": "ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR",
                        "abstract": "The NERC Airborne Research & Survey Facility (ARSF) provides the UK environmental science community with LiDAR (Light Detection and Ranging) data from an Optech ALTM 3033 instrument. The sensor is on loan to the ARSF only for some periods of the year from the Unit of Landscape Modelling (ULM) at Cambridge University"
                    },
                    "relatedTo": {
                        "ob_id": 10828,
                        "uuid": "73d76f0f466f4250a8c6910a53b2d416",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/02 over the Difarsa Area, Nile Gorge, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3826,
                    "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": 10828,
                        "uuid": "73d76f0f466f4250a8c6910a53b2d416",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/02 over the Difarsa Area, Nile Gorge, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3827,
                    "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": 10828,
                        "uuid": "73d76f0f466f4250a8c6910a53b2d416",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, Optech LIDAR and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight ET07/02 over the Difarsa Area, Nile Gorge, Ethiopia",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Optech Airborne Laser Terrain Mapper 3033 LIDAR, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10832,
            "uuid": "6e80d66f267d4b35bd32e2900bc4fb7a",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 97/01 over the South Nottingham Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 1 (CASI-1), ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8692,
                    "uuid": "f6f35b2e9a39416c987e8ff7eca15995",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft",
                    "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3828,
                    "platform": {
                        "ob_id": 8691,
                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
                        "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983."
                    },
                    "instrument": {
                        "ob_id": 8701,
                        "uuid": "0207b70a7b5543de832f5a0d49320cbe",
                        "short_code": "instr",
                        "title": "ARSF Compact Airbone Spectrographic Imager 1 (CASI-1)",
                        "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 1"
                    },
                    "relatedTo": {
                        "ob_id": 10832,
                        "uuid": "6e80d66f267d4b35bd32e2900bc4fb7a",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 97/01 over the South Nottingham Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 1 (CASI-1), ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                },
                {
                    "ob_id": 3829,
                    "platform": {
                        "ob_id": 8691,
                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
                        "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983."
                    },
                    "instrument": {
                        "ob_id": 8754,
                        "uuid": "967ae4b17bf145d8a8a6982a648d64d5",
                        "short_code": "instr",
                        "title": "ARSF Airborne Thematic Mapper (ATM) Daedalus-1268",
                        "abstract": "NERC ARSF Airborne Thematic Mapper Daedalus 1268 instrument. The Daedalus (now ArgonST) 1268 ATM is a passive multispectral scanner providing 11 fixed wavelength position bands in the visible, near, short and thermal infrared. The ATM was purchased by NERC in 1993. The bands approximate those of Landsat. This instrument was operated from 1982 until 1998."
                    },
                    "relatedTo": {
                        "ob_id": 10832,
                        "uuid": "6e80d66f267d4b35bd32e2900bc4fb7a",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 97/01 over the South Nottingham Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 1 (CASI-1), ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                },
                {
                    "ob_id": 3830,
                    "platform": {
                        "ob_id": 8691,
                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
                        "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983."
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10832,
                        "uuid": "6e80d66f267d4b35bd32e2900bc4fb7a",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 97/01 over the South Nottingham Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 1 (CASI-1), ARSF Airborne Thematic Mapper (ATM) Daedalus-1268, ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 10836,
            "uuid": "65ce23b62c694b8bbd5b8e1c08c76e72",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 90/45 over the Winchester Wheat Fields Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8692,
                    "uuid": "f6f35b2e9a39416c987e8ff7eca15995",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Piper PA31 Navajo Chieftain G-NERC Aircraft",
                    "abstract": "Mobile Platform Operation related to the: Piper PA31 Navajo Chieftain G-NERC Aircraft"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3831,
                    "platform": {
                        "ob_id": 8691,
                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
                        "abstract": "A Piper PA31 Navajo Chieftain aircraft converted to survey configuration in 1983."
                    },
                    "instrument": {
                        "ob_id": 8855,
                        "uuid": "675df2bd79404c8ba30c6991111df9e7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC8 Analogue Photographic camera",
                        "abstract": "The Wild (now Leica) RC-10 Aviphot Aerial Camera System is designed for taking near-vertical serial exposures from the air. The standard negative format is 230x230mm. The lens cones may be interchanged during flight if required, giving the RC-10 a very high rating for its versatility and economy. The lenses are colour corrected for the visible and infra red spectral ranges and enable exposures to be made at all the usual scales with various focal lengths up to the operational ceiling of survey aircraft. To align and level the camera during the flight the operator uses the drift sight adjusting remotely the camera attitude and correcting for aircraft roll, pitch and yaw.\r\n"
                    },
                    "relatedTo": {
                        "ob_id": 10836,
                        "uuid": "65ce23b62c694b8bbd5b8e1c08c76e72",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 90/45 over the Winchester Wheat Fields Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC8 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 10840,
            "uuid": "0bd73f0c2bdb4f7aaa92b6ba5b8d2c2e",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/07 over the Inverclyde Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3832,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 7858,
                        "uuid": "ee7d3a6b6a1e4101b58538749b075030",
                        "short_code": "instr",
                        "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)",
                        "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres."
                    },
                    "relatedTo": {
                        "ob_id": 10840,
                        "uuid": "0bd73f0c2bdb4f7aaa92b6ba5b8d2c2e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/07 over the Inverclyde Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3833,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10840,
                        "uuid": "0bd73f0c2bdb4f7aaa92b6ba5b8d2c2e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/07 over the Inverclyde Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3834,
                    "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": 10840,
                        "uuid": "0bd73f0c2bdb4f7aaa92b6ba5b8d2c2e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/07 over the Inverclyde Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3835,
                    "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": 10840,
                        "uuid": "0bd73f0c2bdb4f7aaa92b6ba5b8d2c2e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and AISA Eagle and Hawk Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB07/07 over the Inverclyde Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF WILD-RC10 Analogue Photographic camera, ARSF Specim AISA Hawk, ARSF Specim AISA Eagle; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10844,
            "uuid": "6dcdf744dc5b418fad2669e2a273c99c",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/08 over the Otterburn and Cheviot Hills Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 6410,
                    "uuid": "eb9f0ae42c1c4d87b2bd72543b1be671",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Dornier Do228-101 D-CALM",
                    "abstract": "Mobile Platform Operation related to the: Dornier Do228-101 D-CALM"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3836,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 7858,
                        "uuid": "ee7d3a6b6a1e4101b58538749b075030",
                        "short_code": "instr",
                        "title": "ARSF Compact Airbone Spectrographic Imager 2 (CASI-2)",
                        "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 2 in operation since January 2000. \r\n\r\nThe ItresCompact Airborne Spectrographic Imager (CASI-2) contains a two-dimensional CCD array-based pushbroom imaging spectrograph. The CASI-2 offers a multispectral mode (programmable bands) and a hyperspectral data cube mode. It produces digital geocoded imagery for map registrations, GIS integration, and generates multiple value-added information products from the same set of image data. It operates over a spectral range between 405nm and 950nm and has a 54.4 degree field of view across-track. The CASI-2 is a high spatial and spectral resolution remote sensing sensor. Pixel resolutions can vary from sub-metre to 10 metres."
                    },
                    "relatedTo": {
                        "ob_id": 10844,
                        "uuid": "6dcdf744dc5b418fad2669e2a273c99c",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/08 over the Otterburn and Cheviot Hills Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3837,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8626,
                        "uuid": "c069d0c60e0345b8b37d1c28adfb4db9",
                        "short_code": "instr",
                        "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)",
                        "abstract": "NERC ARSF ATM AZ-16 Airborne Thematic Mapper operated from 1996 to present"
                    },
                    "relatedTo": {
                        "ob_id": 10844,
                        "uuid": "6dcdf744dc5b418fad2669e2a273c99c",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/08 over the Otterburn and Cheviot Hills Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 3838,
                    "platform": {
                        "ob_id": 6394,
                        "uuid": "d2c5c36981824b71a98a2906394d61f3",
                        "short_code": "plat",
                        "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                        "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
                    },
                    "instrument": {
                        "ob_id": 8608,
                        "uuid": "b253208e4d394fb5803379bd0f39dec7",
                        "short_code": "instr",
                        "title": "ARSF WILD-RC10 Analogue Photographic camera",
                        "abstract": "Airborne analogue photographic camera used by the NERC ARSF 199? - 2006. Negatives of frames obtained using this instrument have now been scanned and are available online in JPEG2000 format."
                    },
                    "relatedTo": {
                        "ob_id": 10844,
                        "uuid": "6dcdf744dc5b418fad2669e2a273c99c",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI-2 and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/08 over the Otterburn and Cheviot Hills Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2), ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16), ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 10850,
            "uuid": "fd856944be924c639a40ec4afac871ae",
            "short_code": "acq",
            "title": "Acquisition Process for: Fire Radiative Power from MSG SEVIRI data",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Spinning Enhanced Visible and InfraRed Imager - SEVIRI-1; PLATFORMS: Meteosat Second Generation 2 (MSG-2) or METEOSAT-9; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 2660,
                    "uuid": "c606cf5dba3f4a419cd95d8b4cb52b30",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Meteosat Second Generation 2 (MSG-2) or METEOSAT-9",
                    "abstract": "Mobile Platform Operation related to the: Meteosat Second Generation 2 (MSG-2) or METEOSAT-9"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3839,
                    "platform": {
                        "ob_id": 2658,
                        "uuid": "b61deca60f694b21a49daeec9489f49a",
                        "short_code": "plat",
                        "title": "Meteosat Second Generation 2 (MSG-2) or METEOSAT-9",
                        "abstract": "The second MSG was launched on 21 December 2005 on the same type of launcher as its predecessor - a standard Ariane 5 - from the same launch site - Kourou in French Guiana. It is currently in the same fixed section of orbital space as MSG-1 in geostationary orbit, close to where the equator meets the Greenwich meridian. \nThe reason for the duplication is simply to guarantee continuity of service in case of satellite failure. Weather satellites have become so crucial a part of our daily life that any long gap in service coverage has become inconceivable."
                    },
                    "instrument": {
                        "ob_id": 2651,
                        "uuid": "f16d9f9f95db42b0a1db527ef62c9fdd",
                        "short_code": "instr",
                        "title": "Spinning Enhanced Visible and InfraRed Imager - SEVIRI-1",
                        "abstract": "The Spinning Enhanced Visible and InfraRed Imager (SEVIRI) instrument measures in 12 spectral channels (compared to only 3 on the previous Meteosat) and records data in a 15 minute cycle (30 minutes on the previous Meteosat). The resolution of the high-resolution visible light channel measures 1 km at the sub-satellite point (compared to 2.5 km on the previous Meteosat).\n\nThe first Meteosat Second Generation satellite, MSG-1, came into operational service on 29th January 2004 and was renamed Meteosat-8. MSG-1 has a nominal lifetime of seven years."
                    },
                    "relatedTo": {
                        "ob_id": 10850,
                        "uuid": "fd856944be924c639a40ec4afac871ae",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Fire Radiative Power from MSG SEVIRI data",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Spinning Enhanced Visible and InfraRed Imager - SEVIRI-1; PLATFORMS: Meteosat Second Generation 2 (MSG-2) or METEOSAT-9; "
                    }
                }
            ]
        },
        {
            "ob_id": 10890,
            "uuid": "caccaad558e34b4b9671a53d890c08f0",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from AVHRR-3 at Metop-A for the Eumetsat Polar System Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: AVHRR-3; PLATFORMS: Metop-A; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8209,
                    "uuid": "f0f061d64cca41c3a4221b713fd6b1be",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Metop-A",
                    "abstract": "Mobile Platform Operation related to the: Metop-A"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3840,
                    "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": 10888,
                        "uuid": "174943d1a43c4de4896d799d2b19b4f6",
                        "short_code": "instr",
                        "title": "AVHRR-3",
                        "abstract": "The AVHRR/3, on board the EPS MetOp satellite series, scans the Earth surface in six spectral bands in the range of 0.58 - 12.5 microns. It provides day and night imaging of land, water and clouds, measures sea surface temperature, ice, snow and vegetation cover."
                    },
                    "relatedTo": {
                        "ob_id": 10890,
                        "uuid": "caccaad558e34b4b9671a53d890c08f0",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from AVHRR-3 at Metop-A for the Eumetsat Polar System Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: AVHRR-3; PLATFORMS: Metop-A; "
                    }
                }
            ]
        },
        {
            "ob_id": 10900,
            "uuid": "f980d6776db44e9e87db047c97141345",
            "short_code": "acq",
            "title": "Acquisition Process for: MODIS Surface Reflectance Product from the Terra Satellite (MOD09)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Moderate Resolution Imaging Spectroradiometer (MODIS); PLATFORMS: Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM); ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 10899,
                    "uuid": "9d602cacdc46488499c4490e1e6a4432",
                    "short_code": "mpop",
                    "title": "Terra Satellite orbit details",
                    "abstract": "NASA's Terra (EOS-AM1) is a sun-synchronous, polar orbiting satellite in a morning orbit, with equator crossing times of approximately 10.30 am and 10.30 pm (local solar time) in descending and ascending modes respectively."
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3841,
                    "platform": {
                        "ob_id": 10897,
                        "uuid": "fc7da890b6424fb29bc5aadcda252bf3",
                        "short_code": "plat",
                        "title": "Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM)",
                        "abstract": "Terra, launched on 18th December 1999, is a polar-orbiting satellite within the Morning Constellation that have equator crossings around 10:30 and 22:30 under NASA's Earth Obseration System (EOS).\r\n\r\nOn February 24, 2000, Terra began collecting what was aimed to ultimately become a new, 15-year global data set on which to base scientific investigations about our complex home planet. Together with the entire fleet of EOS spacecraft, Terra is helping scientists unravel the mysteries of climate and environmental change.\r\n\r\nThe satellite carries the Advanced Spaceborne Thermal Emission and Reflection Radiometer (ASTER), the Clouds and Earth's Radiant Energy System (CERES), the Measurements of Pollution in the Troposphere (MOPITT), the Moderate Resolution Imaging Spectroradiometer (MODIS) and the Multi-angle Imaging Spectroradiometer (MISR), and these collect data on the Earth's atmosphere, ocean, land, snow and ice, and energy budget."
                    },
                    "instrument": {
                        "ob_id": 10898,
                        "uuid": "1a661d783a824fe8979faca4b9457fab",
                        "short_code": "instr",
                        "title": "Moderate Resolution Imaging Spectroradiometer (MODIS)",
                        "abstract": "The Moderate Resolution Imaging Spectroradiometer (MODIS) provides high radiometric sensitivity in 36 spectral bands ranging from 0.4 to 14.4 micrometres. Two bands are imaged at a nominal resolution of 250 m at nadir, with five bands at 500 m, and the remaining 29 bands at 1 km. There are two MODIS instruments in operation; one on the Terra satellite and the other on the Aqua satellite, launched in 1999 and 2002 respectively. A +/- 55-degree scanning pattern at the EOS orbit of 705 km, which both satellites are on, results in a 2,330-km swath. Global coverage is provided once every one to two days. "
                    },
                    "relatedTo": {
                        "ob_id": 10900,
                        "uuid": "f980d6776db44e9e87db047c97141345",
                        "short_code": "acq",
                        "title": "Acquisition Process for: MODIS Surface Reflectance Product from the Terra Satellite (MOD09)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Moderate Resolution Imaging Spectroradiometer (MODIS); PLATFORMS: Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM); "
                    }
                }
            ]
        },
        {
            "ob_id": 10908,
            "uuid": "e280896efade4dd3ae8ee6e0b65dcf46",
            "short_code": "acq",
            "title": "Acquisition Process for: MODIS data from the Aqua and Terra Satellites",
            "abstract": "Deployed on Aqua Satellite, part of the Earth Observation System Afternoon Constellation (EOS-PM).  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.\r\n\r\nAqua is the only satellite in the Aqua mission, and it is a part of the Afternoon Constellation, a group of polar-orbiting satellites sharing the same orbit that all have equator crossings around 13:30 and 01:30. The Satellite was launched on 4th April 2002.\r\n\r\nThe Atmospheric Infrared Sounder (AIRS)\r\nThe Advanced Microwave Sounding Unit (AMSU-A)\r\nThe Humidity Sounder for Brazil (HSB)\r\nThe Advanced Microwave Scanning Radiometer for EOS (AMSR-E)\r\nThe Moderate-Resolution Imaging Spectroradiometer (MODIS)\r\nThe Clouds and the Earth's Radiant Energy System (CERES)\r\n\r\nThese instruments collects data on atmospheric conditions, snow and ice, sea surface temperature and ocean productivity and soil moisture.\r\n",
            "imageDetails": [
                128
            ],
            "mobilePlatformOperation": [
                {
                    "ob_id": 10907,
                    "uuid": "1be652a219874193976dff38a64fc180",
                    "short_code": "mpop",
                    "title": "Aqua Satellite orbit details",
                    "abstract": "NASA's AQUA (EOS-PM1) is a sun-synchronous, polar orbiting satellite in an afternoon orbit, with equator crossing times of approximately 13:30 and 01:30.   It forms part of the A-train, a collection of satellites orbiting close together along the same orbital track"
                },
                {
                    "ob_id": 10899,
                    "uuid": "9d602cacdc46488499c4490e1e6a4432",
                    "short_code": "mpop",
                    "title": "Terra Satellite orbit details",
                    "abstract": "NASA's Terra (EOS-AM1) is a sun-synchronous, polar orbiting satellite in a morning orbit, with equator crossing times of approximately 10.30 am and 10.30 pm (local solar time) in descending and ascending modes respectively."
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3842,
                    "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": 10898,
                        "uuid": "1a661d783a824fe8979faca4b9457fab",
                        "short_code": "instr",
                        "title": "Moderate Resolution Imaging Spectroradiometer (MODIS)",
                        "abstract": "The Moderate Resolution Imaging Spectroradiometer (MODIS) provides high radiometric sensitivity in 36 spectral bands ranging from 0.4 to 14.4 micrometres. Two bands are imaged at a nominal resolution of 250 m at nadir, with five bands at 500 m, and the remaining 29 bands at 1 km. There are two MODIS instruments in operation; one on the Terra satellite and the other on the Aqua satellite, launched in 1999 and 2002 respectively. A +/- 55-degree scanning pattern at the EOS orbit of 705 km, which both satellites are on, results in a 2,330-km swath. Global coverage is provided once every one to two days. "
                    },
                    "relatedTo": {
                        "ob_id": 10908,
                        "uuid": "e280896efade4dd3ae8ee6e0b65dcf46",
                        "short_code": "acq",
                        "title": "Acquisition Process for: MODIS data from the Aqua and Terra Satellites",
                        "abstract": "Deployed on Aqua Satellite, part of the Earth Observation System Afternoon Constellation (EOS-PM).  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.\r\n\r\nAqua is the only satellite in the Aqua mission, and it is a part of the Afternoon Constellation, a group of polar-orbiting satellites sharing the same orbit that all have equator crossings around 13:30 and 01:30. The Satellite was launched on 4th April 2002.\r\n\r\nThe Atmospheric Infrared Sounder (AIRS)\r\nThe Advanced Microwave Sounding Unit (AMSU-A)\r\nThe Humidity Sounder for Brazil (HSB)\r\nThe Advanced Microwave Scanning Radiometer for EOS (AMSR-E)\r\nThe Moderate-Resolution Imaging Spectroradiometer (MODIS)\r\nThe Clouds and the Earth's Radiant Energy System (CERES)\r\n\r\nThese instruments collects data on atmospheric conditions, snow and ice, sea surface temperature and ocean productivity and soil moisture.\r\n"
                    }
                },
                {
                    "ob_id": 11762,
                    "platform": {
                        "ob_id": 10897,
                        "uuid": "fc7da890b6424fb29bc5aadcda252bf3",
                        "short_code": "plat",
                        "title": "Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM)",
                        "abstract": "Terra, launched on 18th December 1999, is a polar-orbiting satellite within the Morning Constellation that have equator crossings around 10:30 and 22:30 under NASA's Earth Obseration System (EOS).\r\n\r\nOn February 24, 2000, Terra began collecting what was aimed to ultimately become a new, 15-year global data set on which to base scientific investigations about our complex home planet. Together with the entire fleet of EOS spacecraft, Terra is helping scientists unravel the mysteries of climate and environmental change.\r\n\r\nThe satellite carries the Advanced Spaceborne Thermal Emission and Reflection Radiometer (ASTER), the Clouds and Earth's Radiant Energy System (CERES), the Measurements of Pollution in the Troposphere (MOPITT), the Moderate Resolution Imaging Spectroradiometer (MODIS) and the Multi-angle Imaging Spectroradiometer (MISR), and these collect data on the Earth's atmosphere, ocean, land, snow and ice, and energy budget."
                    },
                    "instrument": {
                        "ob_id": 10898,
                        "uuid": "1a661d783a824fe8979faca4b9457fab",
                        "short_code": "instr",
                        "title": "Moderate Resolution Imaging Spectroradiometer (MODIS)",
                        "abstract": "The Moderate Resolution Imaging Spectroradiometer (MODIS) provides high radiometric sensitivity in 36 spectral bands ranging from 0.4 to 14.4 micrometres. Two bands are imaged at a nominal resolution of 250 m at nadir, with five bands at 500 m, and the remaining 29 bands at 1 km. There are two MODIS instruments in operation; one on the Terra satellite and the other on the Aqua satellite, launched in 1999 and 2002 respectively. A +/- 55-degree scanning pattern at the EOS orbit of 705 km, which both satellites are on, results in a 2,330-km swath. Global coverage is provided once every one to two days. "
                    },
                    "relatedTo": {
                        "ob_id": 10908,
                        "uuid": "e280896efade4dd3ae8ee6e0b65dcf46",
                        "short_code": "acq",
                        "title": "Acquisition Process for: MODIS data from the Aqua and Terra Satellites",
                        "abstract": "Deployed on Aqua Satellite, part of the Earth Observation System Afternoon Constellation (EOS-PM).  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.\r\n\r\nAqua is the only satellite in the Aqua mission, and it is a part of the Afternoon Constellation, a group of polar-orbiting satellites sharing the same orbit that all have equator crossings around 13:30 and 01:30. The Satellite was launched on 4th April 2002.\r\n\r\nThe Atmospheric Infrared Sounder (AIRS)\r\nThe Advanced Microwave Sounding Unit (AMSU-A)\r\nThe Humidity Sounder for Brazil (HSB)\r\nThe Advanced Microwave Scanning Radiometer for EOS (AMSR-E)\r\nThe Moderate-Resolution Imaging Spectroradiometer (MODIS)\r\nThe Clouds and the Earth's Radiant Energy System (CERES)\r\n\r\nThese instruments collects data on atmospheric conditions, snow and ice, sea surface temperature and ocean productivity and soil moisture.\r\n"
                    }
                }
            ]
        },
        {
            "ob_id": 10914,
            "uuid": "a3e54dfef78f4c459685ecada61a8303",
            "short_code": "acq",
            "title": "Acquisition Process for: MODIS Geolocation Data Set from the Terra Satellite (MOD03)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Moderate Resolution Imaging Spectroradiometer (MODIS); PLATFORMS: Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM); ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 10899,
                    "uuid": "9d602cacdc46488499c4490e1e6a4432",
                    "short_code": "mpop",
                    "title": "Terra Satellite orbit details",
                    "abstract": "NASA's Terra (EOS-AM1) is a sun-synchronous, polar orbiting satellite in a morning orbit, with equator crossing times of approximately 10.30 am and 10.30 pm (local solar time) in descending and ascending modes respectively."
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3843,
                    "platform": {
                        "ob_id": 10897,
                        "uuid": "fc7da890b6424fb29bc5aadcda252bf3",
                        "short_code": "plat",
                        "title": "Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM)",
                        "abstract": "Terra, launched on 18th December 1999, is a polar-orbiting satellite within the Morning Constellation that have equator crossings around 10:30 and 22:30 under NASA's Earth Obseration System (EOS).\r\n\r\nOn February 24, 2000, Terra began collecting what was aimed to ultimately become a new, 15-year global data set on which to base scientific investigations about our complex home planet. Together with the entire fleet of EOS spacecraft, Terra is helping scientists unravel the mysteries of climate and environmental change.\r\n\r\nThe satellite carries the Advanced Spaceborne Thermal Emission and Reflection Radiometer (ASTER), the Clouds and Earth's Radiant Energy System (CERES), the Measurements of Pollution in the Troposphere (MOPITT), the Moderate Resolution Imaging Spectroradiometer (MODIS) and the Multi-angle Imaging Spectroradiometer (MISR), and these collect data on the Earth's atmosphere, ocean, land, snow and ice, and energy budget."
                    },
                    "instrument": {
                        "ob_id": 10898,
                        "uuid": "1a661d783a824fe8979faca4b9457fab",
                        "short_code": "instr",
                        "title": "Moderate Resolution Imaging Spectroradiometer (MODIS)",
                        "abstract": "The Moderate Resolution Imaging Spectroradiometer (MODIS) provides high radiometric sensitivity in 36 spectral bands ranging from 0.4 to 14.4 micrometres. Two bands are imaged at a nominal resolution of 250 m at nadir, with five bands at 500 m, and the remaining 29 bands at 1 km. There are two MODIS instruments in operation; one on the Terra satellite and the other on the Aqua satellite, launched in 1999 and 2002 respectively. A +/- 55-degree scanning pattern at the EOS orbit of 705 km, which both satellites are on, results in a 2,330-km swath. Global coverage is provided once every one to two days. "
                    },
                    "relatedTo": {
                        "ob_id": 10914,
                        "uuid": "a3e54dfef78f4c459685ecada61a8303",
                        "short_code": "acq",
                        "title": "Acquisition Process for: MODIS Geolocation Data Set from the Terra Satellite (MOD03)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Moderate Resolution Imaging Spectroradiometer (MODIS); PLATFORMS: Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM); "
                    }
                }
            ]
        },
        {
            "ob_id": 10920,
            "uuid": "d4ffd8b1c9ac41439e90bdb985a24e07",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from ENVISAT AATSR at Envisat for the ENVISAT Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ENVISAT AATSR; PLATFORMS: Envisat; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 848,
                    "uuid": "2efbdc6cb553410a8982ce9d8ee692f2",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Envisat",
                    "abstract": "Mobile Platform Operation related to the: Envisat"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3844,
                    "platform": {
                        "ob_id": 846,
                        "uuid": "47779e22cdc6491a9f7491af866f7080",
                        "short_code": "plat",
                        "title": "Envisat",
                        "abstract": "In March 2002, the European Space Agency launched Envisat, an advanced polar-orbiting Earth observation satellite which provides measurements of the atmosphere, ocean, land, and ice. The Envisat satellite has a payload of 10 instruments that will ensure the continuity of the data measurements of the ESA ERS satellites. Envisat data supports earth science research and allows monitoring of the evolution of environmental and climatic changes.\r\n\r\nLaunch date: 01/03/2002\r\nStatus / projected mission lifetime: Terminated on 08/04/2012\r\nOrbit parameters: 30 km in front of ERS2\r\nNominal altitude: 800 km (same as ERS2, near circular)\r\nOrbit type: near-polar, sun-synchronous\r\nInclination: 98.55 degrees\r\nRepeat period: 35 days\r\nEquatorial crossing time: 10:00 local time (descending node)\r\nSwath width: various\r\nResolution: various"
                    },
                    "instrument": {
                        "ob_id": 8076,
                        "uuid": "87a958e6009c48678f5a0dd73026750a",
                        "short_code": "instr",
                        "title": "ENVISAT AATSR",
                        "abstract": "The ENVISAT AATSR continues the ATSR-1 and ATSR-2 mission data sets of precise sea surface temperature (SST), thereby ensuring the production of a 10 year near-continuous data set from the ERS-1 and ERS-2 missions at the levels of accuracy of 0.3 K or better for climate research. AATSR was launched on board the Envisat satellite on 1st March 2002."
                    },
                    "relatedTo": {
                        "ob_id": 10920,
                        "uuid": "d4ffd8b1c9ac41439e90bdb985a24e07",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from ENVISAT AATSR at Envisat for the ENVISAT Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ENVISAT AATSR; PLATFORMS: Envisat; "
                    }
                }
            ]
        },
        {
            "ob_id": 10924,
            "uuid": "1344b11f69ae43019882a84e0471191b",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from ERS2 ATSR2 at ERS-2 for the ESA ERS Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ERS2 ATSR2; PLATFORMS: ERS-2; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 7814,
                    "uuid": "ae416a28a96049e7bf33ea668c187852",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: ERS-2",
                    "abstract": "Mobile Platform Operation related to the: ERS-2"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3845,
                    "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": 8097,
                        "uuid": "28871807a07f4cadb11bceaa4a4cc568",
                        "short_code": "instr",
                        "title": "ERS2 ATSR2",
                        "abstract": "ATSR-2 was launched as part of the payload of ESA's ERS-1 satellite on 21st April 1995, and was the second instrument in the ATSR series including the along track scanning concept.\r\n\r\nEach ATSR instrument has been designed for exceptional sensitivity and stability of calibration, which are achieved through the incorporation of several innovative features in the instrument design. This design has, among other things, enabled the accurate measurement of sea surface temperature to an accuracy of +/- 0.3K.\r\n\r\nThe ATSR2 is equipped with infrared channels at 1.6um, 3.7um, 10.8 um and 12um to match its predecessor ATSR1 in providing brightness temperatures for measurement of sea-surface temperature and cloud-top temperature. In addition, visible channels at 0.55, 0.67 and 0.87 um for vegatation studies and improved cloud detection were also included on ATSR2. The ATSR2 failed in 2008."
                    },
                    "relatedTo": {
                        "ob_id": 10924,
                        "uuid": "1344b11f69ae43019882a84e0471191b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from ERS2 ATSR2 at ERS-2 for the ESA ERS Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ERS2 ATSR2; PLATFORMS: ERS-2; "
                    }
                }
            ]
        },
        {
            "ob_id": 10928,
            "uuid": "c83c56aeecc0489082083d8dab9397e9",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from ERS1 ATSR1 at ERS-1 for the ESA ERS Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ERS1 ATSR1; PLATFORMS: ERS-1; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 7807,
                    "uuid": "a27cd0df0a124f2ca5873877e21f637e",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: ERS-1",
                    "abstract": "Mobile Platform Operation related to the: ERS-1"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3846,
                    "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": 8063,
                        "uuid": "af0f2ee04eee4d81aadcb6470b503a4e",
                        "short_code": "instr",
                        "title": "Along Track Scanning Radiometer (ATSR-1)",
                        "abstract": "ATSR-1 was launched as part of the payload of ESA's ERS-1 satellite on 17th July 1991, and was the test-bed for the along track scanning concept.\r\n\r\nEach ATSR instrument has been designed for exceptional sensitivity and stability of calibration, which are achieved through the incorporation of several innovative features in the instrument design. This design has, among other things, enabled the accurate measurement of sea surface temperature to an accuracy of +/- 0.3K.\r\n\r\nThe ATSR1 instrument has four channels at wavelengths of 1.6um (visible) and three thermal bands at 3.7um, 11um, and 12um.\r\n\r\nThe ATSR instruments are novel in that they incorporate 2 views into each swath scan.  Satellite measurements of the temperature of the surface of the Earth are inevitably affected by the passage of the radiation through the atmosphere. The dual view design of ATSR makes it possible to estimate and correct for these atmospheric effects. The two views result from the instrument's conical scanning mechanism. Each scan takes readings from the nadir position and then sweeps round to take measurements from a point about 900Km along the satellite's track. A few minutes after acquiring the forward view, the satellite passes over the same spot and takes readings for the nadir view. As the two views of the same scene are taken through different atmospheric path lengths, it is possible to calculate a correction for the effect of atmospheric absorption.\r\n\r\nThe ATSR instruments are also self calibrating.  Rather than relying on pre launch calibration, the ATSR instrument has two on-board black bodies at known temperatures. Radiation from these is measured during each scan and used to provide a continuous re-calibration of the instrument. This makes it possible to determine single channel equivalent temperatures correct to +/- 0.05K."
                    },
                    "relatedTo": {
                        "ob_id": 10928,
                        "uuid": "c83c56aeecc0489082083d8dab9397e9",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from ERS1 ATSR1 at ERS-1 for the ESA ERS Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ERS1 ATSR1; PLATFORMS: ERS-1; "
                    }
                }
            ]
        },
        {
            "ob_id": 10974,
            "uuid": "bc02c85f13f74d4795a0a409e6be73cd",
            "short_code": "acq",
            "title": "Acquisition Process for: MISR Level 2 Aerosol Data (MIL2ASAE)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Multi-angle Imaging SpectroRadiometer (MISR); PLATFORMS: Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM); ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 10899,
                    "uuid": "9d602cacdc46488499c4490e1e6a4432",
                    "short_code": "mpop",
                    "title": "Terra Satellite orbit details",
                    "abstract": "NASA's Terra (EOS-AM1) is a sun-synchronous, polar orbiting satellite in a morning orbit, with equator crossing times of approximately 10.30 am and 10.30 pm (local solar time) in descending and ascending modes respectively."
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3847,
                    "platform": {
                        "ob_id": 10897,
                        "uuid": "fc7da890b6424fb29bc5aadcda252bf3",
                        "short_code": "plat",
                        "title": "Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM)",
                        "abstract": "Terra, launched on 18th December 1999, is a polar-orbiting satellite within the Morning Constellation that have equator crossings around 10:30 and 22:30 under NASA's Earth Obseration System (EOS).\r\n\r\nOn February 24, 2000, Terra began collecting what was aimed to ultimately become a new, 15-year global data set on which to base scientific investigations about our complex home planet. Together with the entire fleet of EOS spacecraft, Terra is helping scientists unravel the mysteries of climate and environmental change.\r\n\r\nThe satellite carries the Advanced Spaceborne Thermal Emission and Reflection Radiometer (ASTER), the Clouds and Earth's Radiant Energy System (CERES), the Measurements of Pollution in the Troposphere (MOPITT), the Moderate Resolution Imaging Spectroradiometer (MODIS) and the Multi-angle Imaging Spectroradiometer (MISR), and these collect data on the Earth's atmosphere, ocean, land, snow and ice, and energy budget."
                    },
                    "instrument": {
                        "ob_id": 10972,
                        "uuid": "374843498e534f23adcdb596ae3ece54",
                        "short_code": "instr",
                        "title": "Multi-angle Imaging SpectroRadiometer (MISR)",
                        "abstract": "The Multi-angle Imaging SpectroRadiometer (MISR) was launced on board the National Aeronautic and Space Administration (NASA) Terra platform in December 1999. It makes simulataneous measurements of reflected solar radation at 9 widely spaced angles in 4 spectral bands in the blue, green, red and near-infrared. By making measurements at various angles the instrument provides improved discrimination of various aerosol types, cloud and surface features."
                    },
                    "relatedTo": {
                        "ob_id": 10974,
                        "uuid": "bc02c85f13f74d4795a0a409e6be73cd",
                        "short_code": "acq",
                        "title": "Acquisition Process for: MISR Level 2 Aerosol Data (MIL2ASAE)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Multi-angle Imaging SpectroRadiometer (MISR); PLATFORMS: Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM); "
                    }
                }
            ]
        },
        {
            "ob_id": 10979,
            "uuid": "84244bf3bd0248ebb9d2ffed4ac1e886",
            "short_code": "acq",
            "title": "Acquisition Process for: MISR Level 2 Land Surface Data (MIL2ASLS)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Multi-angle Imaging SpectroRadiometer (MISR); PLATFORMS: Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM); ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 10899,
                    "uuid": "9d602cacdc46488499c4490e1e6a4432",
                    "short_code": "mpop",
                    "title": "Terra Satellite orbit details",
                    "abstract": "NASA's Terra (EOS-AM1) is a sun-synchronous, polar orbiting satellite in a morning orbit, with equator crossing times of approximately 10.30 am and 10.30 pm (local solar time) in descending and ascending modes respectively."
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3848,
                    "platform": {
                        "ob_id": 10897,
                        "uuid": "fc7da890b6424fb29bc5aadcda252bf3",
                        "short_code": "plat",
                        "title": "Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM)",
                        "abstract": "Terra, launched on 18th December 1999, is a polar-orbiting satellite within the Morning Constellation that have equator crossings around 10:30 and 22:30 under NASA's Earth Obseration System (EOS).\r\n\r\nOn February 24, 2000, Terra began collecting what was aimed to ultimately become a new, 15-year global data set on which to base scientific investigations about our complex home planet. Together with the entire fleet of EOS spacecraft, Terra is helping scientists unravel the mysteries of climate and environmental change.\r\n\r\nThe satellite carries the Advanced Spaceborne Thermal Emission and Reflection Radiometer (ASTER), the Clouds and Earth's Radiant Energy System (CERES), the Measurements of Pollution in the Troposphere (MOPITT), the Moderate Resolution Imaging Spectroradiometer (MODIS) and the Multi-angle Imaging Spectroradiometer (MISR), and these collect data on the Earth's atmosphere, ocean, land, snow and ice, and energy budget."
                    },
                    "instrument": {
                        "ob_id": 10972,
                        "uuid": "374843498e534f23adcdb596ae3ece54",
                        "short_code": "instr",
                        "title": "Multi-angle Imaging SpectroRadiometer (MISR)",
                        "abstract": "The Multi-angle Imaging SpectroRadiometer (MISR) was launced on board the National Aeronautic and Space Administration (NASA) Terra platform in December 1999. It makes simulataneous measurements of reflected solar radation at 9 widely spaced angles in 4 spectral bands in the blue, green, red and near-infrared. By making measurements at various angles the instrument provides improved discrimination of various aerosol types, cloud and surface features."
                    },
                    "relatedTo": {
                        "ob_id": 10979,
                        "uuid": "84244bf3bd0248ebb9d2ffed4ac1e886",
                        "short_code": "acq",
                        "title": "Acquisition Process for: MISR Level 2 Land Surface Data (MIL2ASLS)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Multi-angle Imaging SpectroRadiometer (MISR); PLATFORMS: Terra Satellite, part of the Earth Observation System Morning Constellation (EOS-AM); "
                    }
                }
            ]
        },
        {
            "ob_id": 10990,
            "uuid": "d0ba889ea1814e1f9d93764cded9165c",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from LANDSAT4 MSS at Landsat 4 for the Landsat Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: LANDSAT4 MSS; PLATFORMS: Landsat 4; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8249,
                    "uuid": "e7ef68a94eb048b490026ae3b9133c97",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Landsat 4",
                    "abstract": "Mobile Platform Operation related to the: Landsat 4"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3849,
                    "platform": {
                        "ob_id": 8245,
                        "uuid": "4f1e5569a1ef413083ad244f6f91f2a1",
                        "short_code": "plat",
                        "title": "Landsat 4",
                        "abstract": "As part of the Landsat programme Landsat 4 was launched in July 1982 and was operational until July 1987. It carried Thematic Mapper (TM) and MultiSpectral Scanner (MSS) instruments.\r\n\r\nLaunch date\t7/16/1982 (TM transmission failed 1993)\r\nStatus / projected mission lifetime\tLandsat 5 project end 30/06/2001\r\nOrbit parameters\t99 minutes, 16 day, 233-orbit cycle\r\nNominal altitude\t705 km geo-synchronous\r\nOrbit type\tPolar, sun-synchronous\r\nInclination\t98.2 °\r\nRepeat period\t16 days\r\nEquatorial crossing time\t09.45 local time \r\nSwath width\t183 km"
                    },
                    "instrument": {
                        "ob_id": 10988,
                        "uuid": "6a962562800d4104815f30d41c30bde8",
                        "short_code": "instr",
                        "title": "LANDSAT4 MSS",
                        "abstract": "The Multi-spectral Scanner (MSS) sensors are line-scanning devices observing the earth perpendicular to the orbital track."
                    },
                    "relatedTo": {
                        "ob_id": 10990,
                        "uuid": "d0ba889ea1814e1f9d93764cded9165c",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from LANDSAT4 MSS at Landsat 4 for the Landsat Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: LANDSAT4 MSS; PLATFORMS: Landsat 4; "
                    }
                }
            ]
        },
        {
            "ob_id": 11004,
            "uuid": "44dff51ea10947299e44827d928606f4",
            "short_code": "acq",
            "title": "Acquisition Process for: Temperature, Humidity and Winds near the Tropopause (THAW) FAAM BAE-146 aircraft data",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 53,
                    "uuid": "d7eea365352547a18b58f128b34099f3",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                    "abstract": "Mobile Platform Operation related to the: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3850,
                    "platform": {
                        "ob_id": 51,
                        "uuid": "dda4596d5d374564acf8c79b7a119127",
                        "short_code": "plat",
                        "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                        "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
                    },
                    "instrument": {
                        "ob_id": 1421,
                        "uuid": "049933902a764174b385224ff7f15318",
                        "short_code": "instr",
                        "title": "UNDEFINED instrument associated with platform: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                        "abstract": "This instrument is associated with the platform: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE"
                    },
                    "relatedTo": {
                        "ob_id": 11004,
                        "uuid": "44dff51ea10947299e44827d928606f4",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Temperature, Humidity and Winds near the Tropopause (THAW) FAAM BAE-146 aircraft data",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; "
                    }
                }
            ]
        },
        {
            "ob_id": 11024,
            "uuid": "a70d1a1d8ebd4b8698f5e6407d0ca62f",
            "short_code": "acq",
            "title": "Acquisition Process for: Chilbolton Facility for Atmospheric and Radio Research (CFARR) Direct Visible Radiometer Data",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Chilbolton Facility for Atmospheric and Radio Research (CFARR) Direct Visible radiometer; PLATFORMS: Chilbolton Facility for Atmospheric and Radio Research (CFARR), UK; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3851,
                    "platform": {
                        "ob_id": 817,
                        "uuid": "0d60dd064b6449b09f5c7fd4c41bd693",
                        "short_code": "plat",
                        "title": "NCAS Chilbolton Atmospheric Observatory (CAO)",
                        "abstract": "The National Centre for Atmospheric Science's Chilbolton Atmospheric Observatory, formerly known as the Chilbolton Facility for Atmospheric and Radio Research (CFARR), is hosted by the Science and Technology Facilities Council (STFC) in rural Hampshire in the South of England.  Through a combination of long-term observations and tailored operations it provides national capability for the study of clouds, rainfall, boundary-layer processes and aerosols, and is particularly well suited as a site for hosting field campaigns involving visiting instruments.\r\n\r\nThe CAO site is located one mile south of Chilbolton Village, 6 miles south of Andover, Hampshire. The site was used as an airfield during the Second World War and is relatively flat and slightly elevated above the surrounding area.\r\n\r\nThe observatory operates more than twenty major instruments, many continuously, while others are available on-demand according to user configuration requirements. The portfolio includes a powerful combination of dual-polarisation Doppler radars, lidars, radiometers, and supporting instruments; the continuous round-the-clock operation of lidar and cloud radar instruments at Chilbolton is unique within the UK. These are supplemented by a suite of meteorological instrumentation including rain gauges, and disdrometers.  A multi-wavelength sun photometer provides continuous measurements of aerosol optical depth in clear skies, and contributes to the Aerosol Robotic Network (AERONET).\r\n\r\nThe Chilbolton Advanced Meteorological Radar (CAMRa) is mounted on a 25-metre, fully steerable antenna, and is able to probe clouds and storms with unparalleled sensitivity and resolution. In addition, zenith-pointing polarimetric, Doppler 35 GHz and 94 GHz cloud radars are routinely operated for detailed microphysical studies of cloud processes and cloud climatology.  A transportable, scanning 35 GHz cloud radar system is also hosted at Chilbolton, further enhancing the available capability.\r\n\r\nChilbolton was one of the pilot cloud profiling sites for the CLOUDNET project, and continues to make observations that feed into the Aerosol Clouds and Trace Gases Research Infrastructure (ACTRIS).   Capability at the site will be enhanced in the next few years, with the incorporation of a Raman lidar, with the ambition being for this to form an ACTRIS observational platform for aerosol profiling.\r\n\r\nThe presence (since January 2016) of a Defra air quality monitoring supersite at the observatory site (providing rural background measurements as part of national and transboundary networks) offers the research community further excellent opportunities for intercomparison campaigns and instrument evaluation.\r\n\r\nWIGOS id: \r\n0-826-300-3\r\n0-826-300-4\r\n0-826-300-5\r\n\r\nThe Met Office also operated a boundary layer wind profiler at the site (now operated by NCAS AMOF), for which the site was given a WMO ID 03754."
                    },
                    "instrument": {
                        "ob_id": 11023,
                        "uuid": "feca9dc63c954cc6a4b9bb5aa48fc480",
                        "short_code": "instr",
                        "title": "Chilbolton Facility for Atmospheric and Radio Research (CFARR) Direct Visible radiometer",
                        "abstract": "The Kipp & Zonen CHP1 pyrheliometer uses a thermopile to measure the solar irradiance received from the direction of the sun. It is mounted on a Kipp & Zonen Solys 2 solar tracker to ensure constant pointing in the direction of the sun. It operates in conjunction with pyranometers measuring the total and diffuse solar radiation incident upon a horizontal surface. It is mounted approximately 8 m above ground on the roof of a cabin at the Chilbolton Observatory site."
                    },
                    "relatedTo": {
                        "ob_id": 11024,
                        "uuid": "a70d1a1d8ebd4b8698f5e6407d0ca62f",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Chilbolton Facility for Atmospheric and Radio Research (CFARR) Direct Visible Radiometer Data",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Chilbolton Facility for Atmospheric and Radio Research (CFARR) Direct Visible radiometer; PLATFORMS: Chilbolton Facility for Atmospheric and Radio Research (CFARR), UK; "
                    }
                }
            ]
        },
        {
            "ob_id": 11033,
            "uuid": "5603f4209e2643138444e32eec861084",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Unknown Instruments Suite at Cruise ships of opportunity network for the Carbon Variability studies by Ships of Opportunity (CAVASSOO) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Unknown Instruments Suite; PLATFORMS: Cruise ships of opportunity network; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 11032,
                    "uuid": "56ef3688043f43268382d9d4feec8935",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Cruise ships of opportunity network",
                    "abstract": "Mobile Platform Operation related to the: Cruise ships of opportunity network"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3852,
                    "platform": {
                        "ob_id": 11030,
                        "uuid": "8ef474ebdb7d4b55aa974259362d9c8a",
                        "short_code": "plat",
                        "title": "Cruise ships of opportunity network",
                        "abstract": "The ships of opportunity network for the CArbon VAriability Studies by Ships Of Opportunity (CAVASSOO) includes 4 routes: The Nuka-Arctica line, The Germany-North America line, The UK-Caribbean line and The Spain-Antarctica line.\nThe network is now operational and data are collected on the different lines."
                    },
                    "instrument": {
                        "ob_id": 11031,
                        "uuid": "d96582e9ca7240d6941ee3b5fc548eda",
                        "short_code": "instr",
                        "title": "Unknown Instruments Suite",
                        "abstract": "Suite of instruments used onboard ships of opportunity for the CAVASSOO project."
                    },
                    "relatedTo": {
                        "ob_id": 11033,
                        "uuid": "5603f4209e2643138444e32eec861084",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Unknown Instruments Suite at Cruise ships of opportunity network for the Carbon Variability studies by Ships of Opportunity (CAVASSOO) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Unknown Instruments Suite; PLATFORMS: Cruise ships of opportunity network; "
                    }
                }
            ]
        },
        {
            "ob_id": 11047,
            "uuid": "36a1661ea0484e58957173cbdc85d531",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from ENVISAT GOMOS at Envisat for the ENVISAT Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ENVISAT GOMOS; PLATFORMS: Envisat; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 848,
                    "uuid": "2efbdc6cb553410a8982ce9d8ee692f2",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Envisat",
                    "abstract": "Mobile Platform Operation related to the: Envisat"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3854,
                    "platform": {
                        "ob_id": 846,
                        "uuid": "47779e22cdc6491a9f7491af866f7080",
                        "short_code": "plat",
                        "title": "Envisat",
                        "abstract": "In March 2002, the European Space Agency launched Envisat, an advanced polar-orbiting Earth observation satellite which provides measurements of the atmosphere, ocean, land, and ice. The Envisat satellite has a payload of 10 instruments that will ensure the continuity of the data measurements of the ESA ERS satellites. Envisat data supports earth science research and allows monitoring of the evolution of environmental and climatic changes.\r\n\r\nLaunch date: 01/03/2002\r\nStatus / projected mission lifetime: Terminated on 08/04/2012\r\nOrbit parameters: 30 km in front of ERS2\r\nNominal altitude: 800 km (same as ERS2, near circular)\r\nOrbit type: near-polar, sun-synchronous\r\nInclination: 98.55 degrees\r\nRepeat period: 35 days\r\nEquatorial crossing time: 10:00 local time (descending node)\r\nSwath width: various\r\nResolution: various"
                    },
                    "instrument": {
                        "ob_id": 11045,
                        "uuid": "07925992cfa542c1b3f608e3f57f0969",
                        "short_code": "instr",
                        "title": "ENVISAT GOMOS",
                        "abstract": "GOMOS measures atmospheric constituents by spectral analysis of the spectral bands between 250 nm to 675 nm, 756 nm to 773 nm, and 926 nm to 952 nm. Additionally, two photometers operate in two spectral channels; between 470 nm to 520 nm and 650 nm to 700 nm, respectively."
                    },
                    "relatedTo": {
                        "ob_id": 11047,
                        "uuid": "36a1661ea0484e58957173cbdc85d531",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from ENVISAT GOMOS at Envisat for the ENVISAT Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ENVISAT GOMOS; PLATFORMS: Envisat; "
                    }
                }
            ]
        },
        {
            "ob_id": 11051,
            "uuid": "2ce2edc91f7b4d21bc8c357d8ec76cd7",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Reading University Observatory: Middleton net radiometer at Reading University Atmospheric Observatory for the UTLS-OZONE NERC Research Programme Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Reading University Observatory: Middleton net radiometer; PLATFORMS: Reading University Atmospheric Observatory; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3855,
                    "platform": {
                        "ob_id": 1878,
                        "uuid": "dad6ee58123d405cb3d7afa5f3d29d7d",
                        "short_code": "plat",
                        "title": "University of Reading Atmospheric Observatory",
                        "abstract": "The University of Reading Atmospheric Observatory has been a centre for atmospheric measurements and meteorological observations since 1970, continuing records which began originally at the University College of Reading in 1900. The observatory is situated on the Whiteknights campus (51.442 deg N, 0.938 deg W), near the Earley Gate entrance, at 66m above sea level.\r\nIt is an urban site, located within the town of Reading (population 150, 000).  The site is on a flat piece of land, covered by grass all year round.  As well as traditional meteorological observation and automatic continuous meteorological measurements the site is also used for potential gradient (PG) measurements, leading to a large number of metal posts nearby, including a 10m tower and two 10m poles.\r\n "
                    },
                    "instrument": {
                        "ob_id": 1891,
                        "uuid": "f871f29f08d0479ab71eeef42dc01cc4",
                        "short_code": "instr",
                        "title": "Reading University Observatory: Middleton net radiometer",
                        "abstract": "The Net radiation is found using a Middleton net radiometer."
                    },
                    "relatedTo": {
                        "ob_id": 11051,
                        "uuid": "2ce2edc91f7b4d21bc8c357d8ec76cd7",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Reading University Observatory: Middleton net radiometer at Reading University Atmospheric Observatory for the UTLS-OZONE NERC Research Programme Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Reading University Observatory: Middleton net radiometer; PLATFORMS: Reading University Atmospheric Observatory; "
                    }
                }
            ]
        },
        {
            "ob_id": 11055,
            "uuid": "b1a567437373410a97b6938257503736",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from 120-degree x-wire anemometer in wind tunnel at AASE Radiosonde stations for the A Thermal Climatology of the West Midlands Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 120-degree x-wire anemometer in wind tunnel; PLATFORMS: AASE Radiosonde stations; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3856,
                    "platform": {
                        "ob_id": 5485,
                        "uuid": "4fe6c08861874e23bff371b1da2fc746",
                        "short_code": "plat",
                        "title": "AASE Radiosonde stations",
                        "abstract": "Radiosonde stations located in the AASE region of experiment."
                    },
                    "instrument": {
                        "ob_id": 2875,
                        "uuid": "61e817263d59492f8a28697e9c9077c7",
                        "short_code": "instr",
                        "title": "120-degree x-wire anemometer in wind tunnel",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11055,
                        "uuid": "b1a567437373410a97b6938257503736",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from 120-degree x-wire anemometer in wind tunnel at AASE Radiosonde stations for the A Thermal Climatology of the West Midlands Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 120-degree x-wire anemometer in wind tunnel; PLATFORMS: AASE Radiosonde stations; "
                    }
                }
            ]
        },
        {
            "ob_id": 11061,
            "uuid": "1eb0c3f19f7a4b8085e1c6228e42a14e",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Hemispherical Camera Nikon Coolpix 995 at Harwood Forest, UK for the NCAVEO - Network for Calibration and Validation of EO data Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Hemispherical Camera Nikon Coolpix 995; PLATFORMS: Harwood Forest, UK; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3857,
                    "platform": {
                        "ob_id": 11060,
                        "uuid": "8d0a6a1757b64f0f86086a2b25f4f0a0",
                        "short_code": "plat",
                        "title": "Harwood Forest, UK",
                        "abstract": "Harewood Forest, near the Chilbolton Facility for Atmospheric and radio research, covers 670 hectares of mainly ancient semi-natural woodland and was recorded as a Countryside Heritage Area in June 1989. This site was used during the NCAVEO field experiment in June 2006."
                    },
                    "instrument": {
                        "ob_id": 7905,
                        "uuid": "f7a14a94fc314df594ccd00bce6155db",
                        "short_code": "instr",
                        "title": "Hemispherical Camera Nikon Coolpix 995",
                        "abstract": "Hemispherical camera Nikon Coolpix 995. resolution: 2048 x 1536."
                    },
                    "relatedTo": {
                        "ob_id": 11061,
                        "uuid": "1eb0c3f19f7a4b8085e1c6228e42a14e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Hemispherical Camera Nikon Coolpix 995 at Harwood Forest, UK for the NCAVEO - Network for Calibration and Validation of EO data Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Hemispherical Camera Nikon Coolpix 995; PLATFORMS: Harwood Forest, UK; "
                    }
                }
            ]
        },
        {
            "ob_id": 11075,
            "uuid": "f7d26d6bea01465cb2729101d64ee8a2",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from CNR/IMAA (Tito Scalo, Italy): Ceilometer at Alert, Canada",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: CNR/IMAA (Tito Scalo, Italy): Ceilometer; PLATFORMS: Alert, Canada; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3859,
                    "platform": {
                        "ob_id": 5378,
                        "uuid": "08df74d066184d7e9ba31215e043875f",
                        "short_code": "plat",
                        "title": "Alert, Canada",
                        "abstract": "Platform.abstract: DETAILS NEEDED"
                    },
                    "instrument": {
                        "ob_id": 11074,
                        "uuid": "15f95f4732e94918b49b5fb51c7a2547",
                        "short_code": "instr",
                        "title": "CNR/IMAA (Tito Scalo, Italy): Ceilometer",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11075,
                        "uuid": "f7d26d6bea01465cb2729101d64ee8a2",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from CNR/IMAA (Tito Scalo, Italy): Ceilometer at Alert, Canada",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: CNR/IMAA (Tito Scalo, Italy): Ceilometer; PLATFORMS: Alert, Canada; "
                    }
                }
            ]
        },
        {
            "ob_id": 11083,
            "uuid": "9ac98c23b6f549fa82e55f7f1bba70fc",
            "short_code": "acq",
            "title": "Acquisition Process for: VISSR data on GMS-5 for 1995-2001",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Visible and Infrared Spin-Scan Radiometer (VISSR); PLATFORMS: Geostationary Meteorological Satellite (GMS-5); ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 1839,
                    "uuid": "7ff8bf82dfe544e9b53bde5939e2e3fa",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Geostationary Meteorological Satellite (GMS-5)",
                    "abstract": "Mobile Platform Operation related to the: Geostationary Meteorological Satellite (GMS-5)"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 4803,
                    "platform": {
                        "ob_id": 1838,
                        "uuid": "2638ad94d1a941bd80871782c0ca8a7f",
                        "short_code": "plat",
                        "title": "Geostationary Meteorological Satellite (GMS-5)",
                        "abstract": "Japanese Geostationary Meteorological Satellite, also known as its nickname, \"Himawari\" (meaning a \"sunflower\") which carried out weather observation from space being part of the World Weather Watch (WWW) project of the World Meteorological Organization. It was launched on March 18, 1995."
                    },
                    "instrument": {
                        "ob_id": 1701,
                        "uuid": "e005c747944044deb9daf961654b03f3",
                        "short_code": "instr",
                        "title": "Visible and Infrared Spin-Scan Radiometer (VISSR)",
                        "abstract": "Visible and Infrared Spin-Scan Radiometer (VISSR) flown on the SMS-1 and -2 and the GOES-1, -2 and -3. The VISSR provides data to produce photographic displays for the National Weather Service (NWS).  These data allow day/night cloud mapping, surface temperature determination, atmospheric temperature determination, weather forecasting, and meteorological research."
                    },
                    "relatedTo": {
                        "ob_id": 11083,
                        "uuid": "9ac98c23b6f549fa82e55f7f1bba70fc",
                        "short_code": "acq",
                        "title": "Acquisition Process for: VISSR data on GMS-5 for 1995-2001",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Visible and Infrared Spin-Scan Radiometer (VISSR); PLATFORMS: Geostationary Meteorological Satellite (GMS-5); "
                    }
                }
            ]
        },
        {
            "ob_id": 11090,
            "uuid": "832481b55aee43a4801e341e3255dbef",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from FAAM/BAE systems or other aircraft: Flight summary for the Joint Airborne IASI Validation Experiment (JAIVEX) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: FAAM/BAE systems or other aircraft: Flight summary; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": []
        },
        {
            "ob_id": 11094,
            "uuid": "9f274f31e54c4a6aa688158bbc9d182c",
            "short_code": "acq",
            "title": "Acquisition Process for: VISSR data on GOES-8 for 1995-2001",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Visible and Infrared Spin-Scan Radiometer (VISSR); PLATFORMS: Geostationary Operational Environmental Satellite - GOES-8; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 1773,
                    "uuid": "2e481c8868cf4c1bbefd5f1c8f6ad9d1",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Geostationary Operational Environmental Satellite - GOES-8",
                    "abstract": "Mobile Platform Operation related to the: Geostationary Operational Environmental Satellite - GOES-8"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 4802,
                    "platform": {
                        "ob_id": 1772,
                        "uuid": "d37c0d0050be467685e0df338fc68d2a",
                        "short_code": "plat",
                        "title": "Geostationary Operational Environmental Satellite - GOES-8",
                        "abstract": "NASA geostationary weather satellite which was launched on April 13, 1994 and is still operational to this date."
                    },
                    "instrument": {
                        "ob_id": 1701,
                        "uuid": "e005c747944044deb9daf961654b03f3",
                        "short_code": "instr",
                        "title": "Visible and Infrared Spin-Scan Radiometer (VISSR)",
                        "abstract": "Visible and Infrared Spin-Scan Radiometer (VISSR) flown on the SMS-1 and -2 and the GOES-1, -2 and -3. The VISSR provides data to produce photographic displays for the National Weather Service (NWS).  These data allow day/night cloud mapping, surface temperature determination, atmospheric temperature determination, weather forecasting, and meteorological research."
                    },
                    "relatedTo": {
                        "ob_id": 11094,
                        "uuid": "9f274f31e54c4a6aa688158bbc9d182c",
                        "short_code": "acq",
                        "title": "Acquisition Process for: VISSR data on GOES-8 for 1995-2001",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Visible and Infrared Spin-Scan Radiometer (VISSR); PLATFORMS: Geostationary Operational Environmental Satellite - GOES-8; "
                    }
                }
            ]
        },
        {
            "ob_id": 11099,
            "uuid": "76af9552e099478c8cee7cc1a71f3c6b",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from REMOVE -DUPLICATE Met Office - Airborne Research Interferometer Evaluation System (ARIES) at Met Office C-130 Hercules Aircraft for the VIRTEM Validation of IASI Radiative Transfer: Experiments and Modelling Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: Met Office C-130 Hercules Aircraft; PLATFORMS: Met Office C-130 Hercules Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 436,
                    "uuid": "aff5b408066748939fa37a3ca74dc376",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Met Office C-130 Hercules Aircraft",
                    "abstract": "Mobile Platform Operation related to the: Met Office C-130 Hercules Aircraft"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3863,
                    "platform": {
                        "ob_id": 434,
                        "uuid": "f1971a20238b4f5bba4126996bd2816d",
                        "short_code": "plat",
                        "title": "Met Office C-130 Hercules Aircraft",
                        "abstract": "From 1972 to 2001 the Meteorological Research Flight (MRF) operated a C-130 aircraft which was comprehensively equipped to make a wide variety of atmospheric observations. It had been heavily modified for this role and was one of the most sophisticated 'flying laboratories' for atmospheric research in the world. The long striped probe on the nose allows sensitive instruments to make measurements, for example of turbulence, in a region outside the influence of the aircraft itself; it also gives the aircraft its nickname of 'Snoopy'."
                    },
                    "instrument": {
                        "ob_id": 11098,
                        "uuid": "1203cd7ee08d4044a94c507f78ebb564",
                        "short_code": "instr",
                        "title": "UNDEFINED instrument associated with platform: Met Office C-130 Hercules Aircraft",
                        "abstract": "This instrument is associated with the platform: Met Office C-130 Hercules Aircraft"
                    },
                    "relatedTo": {
                        "ob_id": 11099,
                        "uuid": "76af9552e099478c8cee7cc1a71f3c6b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from REMOVE -DUPLICATE Met Office - Airborne Research Interferometer Evaluation System (ARIES) at Met Office C-130 Hercules Aircraft for the VIRTEM Validation of IASI Radiative Transfer: Experiments and Modelling Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: Met Office C-130 Hercules Aircraft; PLATFORMS: Met Office C-130 Hercules Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 11102,
            "uuid": "bda4703d7b2645d8b5ee1ed85ee093f7",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Solar Backscatter UltraViolet (SBUV) Instrument at NIMBUS 7 Satellite for the NASA - National Aeronautics and Space Administration",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Solar Backscatter UltraViolet (SBUV) Instrument; PLATFORMS: NIMBUS 7 Satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 460,
                    "uuid": "bea2c6443d2f4f81a2701f09cb4e6f5c",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: NIMBUS 7 Satellite",
                    "abstract": "Mobile Platform Operation related to the: NIMBUS 7 Satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3864,
                    "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": 1280,
                        "uuid": "018ead43621a462c843078fd0caf48d1",
                        "short_code": "instr",
                        "title": "Solar Backscatter UltraViolet (SBUV) Instrument",
                        "abstract": "The SBUV onboard NIMBUS-7 is an remote sensor designed to map total ozone concentrations and the vertical distribution of ozone in the earth's atmosphere on a global scale. The purpose of the SBUV instrument is to provide data on an operational basis, from which the distribution of ozone can be determined on the ground."
                    },
                    "relatedTo": {
                        "ob_id": 11102,
                        "uuid": "bda4703d7b2645d8b5ee1ed85ee093f7",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Solar Backscatter UltraViolet (SBUV) Instrument at NIMBUS 7 Satellite for the NASA - National Aeronautics and Space Administration",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Solar Backscatter UltraViolet (SBUV) Instrument; PLATFORMS: NIMBUS 7 Satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 11107,
            "uuid": "1e0b9cd3955c4c248e609a1177bbf337",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Ozonesondes at Global ozonesondes network for the Meteorological Services of Canada (MSC) Collection",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Ozonesondes; PLATFORMS: Global ozonesondes network; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3865,
                    "platform": {
                        "ob_id": 1279,
                        "uuid": "27eeb3db71684027ba1c4b02d69da2fc",
                        "short_code": "plat",
                        "title": "Global ozonesondes network",
                        "abstract": "Platform.abstract: DETAILS NEEDED"
                    },
                    "instrument": {
                        "ob_id": 1165,
                        "uuid": "2de713c15aa4490282020cdf9f0b4a46",
                        "short_code": "instr",
                        "title": "Ozonesondes",
                        "abstract": "The ozonesonde is a lightweight, balloon-borne instrument that measures profiles of ozone, pressure, temperature and humidity from the ground to approximately 40km."
                    },
                    "relatedTo": {
                        "ob_id": 11107,
                        "uuid": "1e0b9cd3955c4c248e609a1177bbf337",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Ozonesondes at Global ozonesondes network for the Meteorological Services of Canada (MSC) Collection",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Ozonesondes; PLATFORMS: Global ozonesondes network; "
                    }
                }
            ]
        },
        {
            "ob_id": 11113,
            "uuid": "ff76c59b03604ee59a2823959ae1fe99",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Met Office - Telemetered tipping bucket raingauges at Brownhills Farm, UK for the Natural Environment Research Council (NERC)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office - Telemetered tipping bucket raingauges; PLATFORMS: Brownhills Farm, UK; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3866,
                    "platform": {
                        "ob_id": 7480,
                        "uuid": "f41c7389cb5a43b89e4e2a8b08716c4a",
                        "short_code": "plat",
                        "title": "Brownhills Farm, UK",
                        "abstract": "Raingauge \r\nNational Grid reference 3761 4104"
                    },
                    "instrument": {
                        "ob_id": 6458,
                        "uuid": "25003d5874064f929dbf14708dee4db4",
                        "short_code": "instr",
                        "title": "Met Office - Telemetered tipping bucket raingauges",
                        "abstract": "The tipping bucket raingauge is particularly suitable for the automation of rainfall measurement"
                    },
                    "relatedTo": {
                        "ob_id": 11113,
                        "uuid": "ff76c59b03604ee59a2823959ae1fe99",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Met Office - Telemetered tipping bucket raingauges at Brownhills Farm, UK for the Natural Environment Research Council (NERC)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office - Telemetered tipping bucket raingauges; PLATFORMS: Brownhills Farm, UK; "
                    }
                }
            ]
        },
        {
            "ob_id": 11116,
            "uuid": "d0e23aa8452c4851ba59d3808c448410",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Reading University Observatory: Ground heat flux plate at Reading University Atmospheric Observatory for the UTLS-OZONE NERC Research Programme Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Reading University Observatory: Ground heat flux plate; PLATFORMS: Reading University Atmospheric Observatory; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3867,
                    "platform": {
                        "ob_id": 1878,
                        "uuid": "dad6ee58123d405cb3d7afa5f3d29d7d",
                        "short_code": "plat",
                        "title": "University of Reading Atmospheric Observatory",
                        "abstract": "The University of Reading Atmospheric Observatory has been a centre for atmospheric measurements and meteorological observations since 1970, continuing records which began originally at the University College of Reading in 1900. The observatory is situated on the Whiteknights campus (51.442 deg N, 0.938 deg W), near the Earley Gate entrance, at 66m above sea level.\r\nIt is an urban site, located within the town of Reading (population 150, 000).  The site is on a flat piece of land, covered by grass all year round.  As well as traditional meteorological observation and automatic continuous meteorological measurements the site is also used for potential gradient (PG) measurements, leading to a large number of metal posts nearby, including a 10m tower and two 10m poles.\r\n "
                    },
                    "instrument": {
                        "ob_id": 1887,
                        "uuid": "dddffa9f689c483a99cd24e88549c2f0",
                        "short_code": "instr",
                        "title": "Reading University Observatory: Ground heat flux plate",
                        "abstract": "Ground heat flux is determined using a ground heat flux plate."
                    },
                    "relatedTo": {
                        "ob_id": 11116,
                        "uuid": "d0e23aa8452c4851ba59d3808c448410",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Reading University Observatory: Ground heat flux plate at Reading University Atmospheric Observatory for the UTLS-OZONE NERC Research Programme Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Reading University Observatory: Ground heat flux plate; PLATFORMS: Reading University Atmospheric Observatory; "
                    }
                }
            ]
        },
        {
            "ob_id": 11120,
            "uuid": "b2dd26494a904a61a31b5c9aa42a669c",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from SME Ozone spectrometer at Solar Mesosphere Explorer (SME) satellite for the NASA - National Aeronautics and Space Administration",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SME Ozone spectrometer; PLATFORMS: Solar Mesosphere Explorer (SME) satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 1282,
                    "uuid": "35108dac7cbf4c41992d80c249403c0c",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Solar Mesosphere Explorer (SME) satellite",
                    "abstract": "Mobile Platform Operation related to the: Solar Mesosphere Explorer (SME) satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3868,
                    "platform": {
                        "ob_id": 1278,
                        "uuid": "50df0e3b16ec4effb22ff8426ba31fa5",
                        "short_code": "plat",
                        "title": "Solar Mesosphere Explorer (SME) satellite",
                        "abstract": "A NASA scientific satellite launched on October 6th, 1981 and designed to investigate the processes that create and destroy ozone in Earth's upper atmosphere."
                    },
                    "instrument": {
                        "ob_id": 1281,
                        "uuid": "2b83bcdcc1c74896b5badd2d1bd85a33",
                        "short_code": "instr",
                        "title": "SME Ozone spectrometer",
                        "abstract": "Ozone spectrometer onboard the Stratospheric Mesosphere Explorer satellite."
                    },
                    "relatedTo": {
                        "ob_id": 11120,
                        "uuid": "b2dd26494a904a61a31b5c9aa42a669c",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from SME Ozone spectrometer at Solar Mesosphere Explorer (SME) satellite for the NASA - National Aeronautics and Space Administration",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SME Ozone spectrometer; PLATFORMS: Solar Mesosphere Explorer (SME) satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 11124,
            "uuid": "e8c22a629386446a83d6fed54ed64838",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from UEA: condensation nuclei counter at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UEA: condensation nuclei counter; PLATFORMS: Jungfraujoch, Switzerland; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3869,
                    "platform": {
                        "ob_id": 1523,
                        "uuid": "97bdfb9741f441eebfb16440ebbb0f92",
                        "short_code": "plat",
                        "title": "Jungfraujoch Research Station",
                        "abstract": "The high altitude research station Jungfraujoch (7° 59' E, 46° 32' N, 3580 m a.s.l.) is situated on a mountain saddle in the central Swiss Alps between the Jungfrau (4158 m a.s.l.) in the West and the Moench (4099 m a.s.l.) in the East. The International Foundation High Altitude Research Stations Jungfraujoch and Gornergrat (HFSJG) runs the research station and provides the infrastructure and support for scientific research. Due to its unique place, the year-round accessibility, and the excellent infrastructure, the Jungfraujoch research station is well suited for long-term ground-based monitoring of trace gas concentrations trends in the free troposphere. Due to its location in central Europe and its proximity to anthropogenic greenhouse gas source regions it is also an appropriate study site for European regional source allocations during pollution events. The research activities of EMPA at the Jungfraujoch are conducted within the scope of the Swiss National Air Pollution Monitoring Network (NABEL) funded by the Swiss Federal Office for the Environment (FOEN) and the Global Atmosphere Watch Program (GAW) of the World Meteorological Organization (WMO). The measurement programme at Jungfraujoch includes continuous in-situ analyses of ozone (O3), carbon monoxide (CO), nitrogen monoxide (NO), nitrogen dioxide (NO2), and the sum of nitrogen oxides (NOy). In addition, an extended set of halocarbons and a selection of VOCs (alkanes, aromatics) are measured with a time resolution of four hours since 2000 as a part of SOGE. Daily samples are taken for determination of gaseous SO2 and for particulate sulphur. The concentrations of total suspended particles are continuously observed as well as measured as 48-hour bulk samples. Measurements of methane, nitrous oxide and sulphur hexafluoride were commenced in February 2005 funded by the FOEN. Therefore, the whole set of non-CO2 greenhouse gases is now continuously monitored at the Jungfraujoch."
                    },
                    "instrument": {
                        "ob_id": 2922,
                        "uuid": "a962d4cde17e494a85851ddf89abec47",
                        "short_code": "instr",
                        "title": "UEA: condensation nuclei counter",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11124,
                        "uuid": "e8c22a629386446a83d6fed54ed64838",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from UEA: condensation nuclei counter at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UEA: condensation nuclei counter; PLATFORMS: Jungfraujoch, Switzerland; "
                    }
                }
            ]
        },
        {
            "ob_id": 11128,
            "uuid": "db35cfa64d8d466a880c08168924bfcd",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from REMOVE - CASLab automatic weather station at Halley Clean Air Sector Laboratory (CASLab) for the Chemistry of the Antarctic Boundary Layer and the Interface with Snow (CHABLIS) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: Halley Clean Air Sector Laboratory (CASLab); PLATFORMS: Halley Clean Air Sector Laboratory (CASLab); ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3870,
                    "platform": {
                        "ob_id": 719,
                        "uuid": "f9b6a7829ae1429c92677ff67b9e5df1",
                        "short_code": "plat",
                        "title": "Halley Clean Air Sector Laboratory (CASLab)",
                        "abstract": "The Clean Air Sector Laboratory (CASLab) is located 1km from the Halley station in Antarctica and is dedicated to studies of atmospheric chemistry, air/snow exchange and boundary layer meteorology."
                    },
                    "instrument": {
                        "ob_id": 11127,
                        "uuid": "3a394f5ebe3948368567da7cb905106b",
                        "short_code": "instr",
                        "title": "UNDEFINED instrument associated with platform: Halley Clean Air Sector Laboratory (CASLab)",
                        "abstract": "This instrument is associated with the platform: Halley Clean Air Sector Laboratory (CASLab)"
                    },
                    "relatedTo": {
                        "ob_id": 11128,
                        "uuid": "db35cfa64d8d466a880c08168924bfcd",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from REMOVE - CASLab automatic weather station at Halley Clean Air Sector Laboratory (CASLab) for the Chemistry of the Antarctic Boundary Layer and the Interface with Snow (CHABLIS) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: Halley Clean Air Sector Laboratory (CASLab); PLATFORMS: Halley Clean Air Sector Laboratory (CASLab); "
                    }
                }
            ]
        },
        {
            "ob_id": 11131,
            "uuid": "cb6cd470a0a5418bac7e1f00234277a0",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from NERC: Mesosphere-Stratosphere-Troposphere (MST) Radar at Aberystwyth, UK for the Natural Environment Research Council (NERC)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: NERC: Mesosphere-Stratosphere-Troposphere (MST) Radar; PLATFORMS: Aberystwyth, UK; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3871,
                    "platform": {
                        "ob_id": 1614,
                        "uuid": "78413160c82e4e8ebda9c036c2a6fa33",
                        "short_code": "plat",
                        "title": "Aberystwyth, UK",
                        "abstract": "Platform.abstract: DETAILS NEEDED"
                    },
                    "instrument": {
                        "ob_id": 6120,
                        "uuid": "6fcd4e23841b4aa0af75b8bb783011ea",
                        "short_code": "instr",
                        "title": "NERC: Mesosphere-Stratosphere-Troposphere (MST) Radar",
                        "abstract": "The NERC MST (Mesosphere-Stratosphere-Troposphere) Radar is a 46.5 MHz pulsed Doppler radar located at Capel Dewi, near Aberystwyth in west Wales. It is the UK's most powerful and versatile wind-profiling instrument. It is operated predominantly in the ST mode, covering the altitude range 2 - 20 km, for which MST radars are unique in their ability to give continuous measurements of the three-dimensional wind vector at high resolution - typically 300 m in altitude and 2 - 3 minutes in time. Moreover, under certain circumstances, it can provide information about atmospheric stability, turbulence and precipitation. It is therefore ideally suited for studying everything from large scale weather systems down to small-scale atmospheric phenomena.\r\n\r\nThe radar began operations in 1990 and has been operated on a quasi-continuous basis since 1997."
                    },
                    "relatedTo": {
                        "ob_id": 11131,
                        "uuid": "cb6cd470a0a5418bac7e1f00234277a0",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from NERC: Mesosphere-Stratosphere-Troposphere (MST) Radar at Aberystwyth, UK for the Natural Environment Research Council (NERC)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: NERC: Mesosphere-Stratosphere-Troposphere (MST) Radar; PLATFORMS: Aberystwyth, UK; "
                    }
                }
            ]
        },
        {
            "ob_id": 11134,
            "uuid": "fdf60782b72848019780962c1d974007",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Full tide bubbler gauge at GLOSS station network",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Full tide bubbler gauge; PLATFORMS: GLOSS station network; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3872,
                    "platform": {
                        "ob_id": 6622,
                        "uuid": "ce0040e923c04c90b75c12cab962d27f",
                        "short_code": "plat",
                        "title": "GLOSS station network",
                        "abstract": "The main component of GLOSS is the 'Global Core Network' (GCN) of 290 sea level stations around the world for long term climate change and oceanographic sea level monitoring."
                    },
                    "instrument": {
                        "ob_id": 6623,
                        "uuid": "180b25d50f47430d964f1cc31fd8a50c",
                        "short_code": "instr",
                        "title": "Full tide bubbler gauge",
                        "abstract": "A type of gauge to measure sea levels."
                    },
                    "relatedTo": {
                        "ob_id": 11134,
                        "uuid": "fdf60782b72848019780962c1d974007",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Full tide bubbler gauge at GLOSS station network",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Full tide bubbler gauge; PLATFORMS: GLOSS station network; "
                    }
                }
            ]
        },
        {
            "ob_id": 11140,
            "uuid": "09ff24da38fb4307a6dd5dd7e242326f",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from NERC MST site : NERC Campbell Scientific Climate data logger at Aberystwyth, UK for the Natural Environment Research Council (NERC)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: NERC MST site : NERC Campbell Scientific Climate data logger; PLATFORMS: Aberystwyth, UK; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3873,
                    "platform": {
                        "ob_id": 1614,
                        "uuid": "78413160c82e4e8ebda9c036c2a6fa33",
                        "short_code": "plat",
                        "title": "Aberystwyth, UK",
                        "abstract": "Platform.abstract: DETAILS NEEDED"
                    },
                    "instrument": {
                        "ob_id": 6124,
                        "uuid": "21d599eda1684cc2b8b55736fe2569b5",
                        "short_code": "instr",
                        "title": "NERC MST site : NERC Campbell Scientific Climate data logger",
                        "abstract": "Meteorological surface observations are recorded at the MST site near Aberystwyth with a (Met Office approved) CR10 \"Climate Data Logger\" from Campbell Scientific."
                    },
                    "relatedTo": {
                        "ob_id": 11140,
                        "uuid": "09ff24da38fb4307a6dd5dd7e242326f",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from NERC MST site : NERC Campbell Scientific Climate data logger at Aberystwyth, UK for the Natural Environment Research Council (NERC)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: NERC MST site : NERC Campbell Scientific Climate data logger; PLATFORMS: Aberystwyth, UK; "
                    }
                }
            ]
        },
        {
            "ob_id": 11143,
            "uuid": "079eff5c14a546fab4f1d9ee734f23f3",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments at FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE for the Aerosol Direct Radiative Impact Experiment (ADRIEX) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments; PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 53,
                    "uuid": "d7eea365352547a18b58f128b34099f3",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                    "abstract": "Mobile Platform Operation related to the: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 5287,
                    "platform": {
                        "ob_id": 51,
                        "uuid": "dda4596d5d374564acf8c79b7a119127",
                        "short_code": "plat",
                        "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                        "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
                    },
                    "instrument": {
                        "ob_id": 61,
                        "uuid": "306ac6a158514192baf813b4b8b46be7",
                        "short_code": "instr",
                        "title": "FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments",
                        "abstract": "Core instruments are provided and can be operated by FAAM. Data will be made available routinely at BADC. Some core instruments may not be operated on all flights. The standard core instrument data may, in some cases, be enhanced (e.g. provided at higher frequency or with greater accuracy) by collaboration with another group."
                    },
                    "relatedTo": {
                        "ob_id": 11143,
                        "uuid": "079eff5c14a546fab4f1d9ee734f23f3",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments at FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE for the Aerosol Direct Radiative Impact Experiment (ADRIEX) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: FAAM/BAE (Facility for Airborne Atmospheric Measurements/British AErospace) systems: Set of FAAM core instruments; PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; "
                    }
                }
            ]
        },
        {
            "ob_id": 11146,
            "uuid": "9ee93efa45ce495a8171defe3673a160",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Pressure transducer at GLOSS station network",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Pressure transducer; PLATFORMS: GLOSS station network; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3875,
                    "platform": {
                        "ob_id": 6622,
                        "uuid": "ce0040e923c04c90b75c12cab962d27f",
                        "short_code": "plat",
                        "title": "GLOSS station network",
                        "abstract": "The main component of GLOSS is the 'Global Core Network' (GCN) of 290 sea level stations around the world for long term climate change and oceanographic sea level monitoring."
                    },
                    "instrument": {
                        "ob_id": 6639,
                        "uuid": "b3ae1cc037564223b9a4b2cc4140a346",
                        "short_code": "instr",
                        "title": "Pressure transducer",
                        "abstract": "Type of tide gauge to measure sea levels."
                    },
                    "relatedTo": {
                        "ob_id": 11146,
                        "uuid": "9ee93efa45ce495a8171defe3673a160",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Pressure transducer at GLOSS station network",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Pressure transducer; PLATFORMS: GLOSS station network; "
                    }
                }
            ]
        },
        {
            "ob_id": 11149,
            "uuid": "28f1cc63191c4c609a586169b8c75110",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Reading University Observatory:  Kipp solarimeters at Reading University Atmospheric Observatory for the UTLS-OZONE NERC Research Programme Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Reading University Observatory:  Kipp solarimeters; PLATFORMS: Reading University Atmospheric Observatory; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3876,
                    "platform": {
                        "ob_id": 1878,
                        "uuid": "dad6ee58123d405cb3d7afa5f3d29d7d",
                        "short_code": "plat",
                        "title": "University of Reading Atmospheric Observatory",
                        "abstract": "The University of Reading Atmospheric Observatory has been a centre for atmospheric measurements and meteorological observations since 1970, continuing records which began originally at the University College of Reading in 1900. The observatory is situated on the Whiteknights campus (51.442 deg N, 0.938 deg W), near the Earley Gate entrance, at 66m above sea level.\r\nIt is an urban site, located within the town of Reading (population 150, 000).  The site is on a flat piece of land, covered by grass all year round.  As well as traditional meteorological observation and automatic continuous meteorological measurements the site is also used for potential gradient (PG) measurements, leading to a large number of metal posts nearby, including a 10m tower and two 10m poles.\r\n "
                    },
                    "instrument": {
                        "ob_id": 1879,
                        "uuid": "2befcc3f5d4747989ad9246316431885",
                        "short_code": "instr",
                        "title": "Reading University Observatory:  Kipp solarimeters",
                        "abstract": "The solar radiation is measured using two Kipp solarimeters, one of which measures the global solar radiation (Sg) and the other measures the diffuse solar component (Sd) by using a shade ring."
                    },
                    "relatedTo": {
                        "ob_id": 11149,
                        "uuid": "28f1cc63191c4c609a586169b8c75110",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Reading University Observatory:  Kipp solarimeters at Reading University Atmospheric Observatory for the UTLS-OZONE NERC Research Programme Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Reading University Observatory:  Kipp solarimeters; PLATFORMS: Reading University Atmospheric Observatory; "
                    }
                }
            ]
        },
        {
            "ob_id": 11152,
            "uuid": "84b7039a77644e048508ca384935b4ef",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from EMPA: UV absorption TEI49C at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: EMPA: UV absorption TEI49C; PLATFORMS: Jungfraujoch, Switzerland; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3877,
                    "platform": {
                        "ob_id": 1523,
                        "uuid": "97bdfb9741f441eebfb16440ebbb0f92",
                        "short_code": "plat",
                        "title": "Jungfraujoch Research Station",
                        "abstract": "The high altitude research station Jungfraujoch (7° 59' E, 46° 32' N, 3580 m a.s.l.) is situated on a mountain saddle in the central Swiss Alps between the Jungfrau (4158 m a.s.l.) in the West and the Moench (4099 m a.s.l.) in the East. The International Foundation High Altitude Research Stations Jungfraujoch and Gornergrat (HFSJG) runs the research station and provides the infrastructure and support for scientific research. Due to its unique place, the year-round accessibility, and the excellent infrastructure, the Jungfraujoch research station is well suited for long-term ground-based monitoring of trace gas concentrations trends in the free troposphere. Due to its location in central Europe and its proximity to anthropogenic greenhouse gas source regions it is also an appropriate study site for European regional source allocations during pollution events. The research activities of EMPA at the Jungfraujoch are conducted within the scope of the Swiss National Air Pollution Monitoring Network (NABEL) funded by the Swiss Federal Office for the Environment (FOEN) and the Global Atmosphere Watch Program (GAW) of the World Meteorological Organization (WMO). The measurement programme at Jungfraujoch includes continuous in-situ analyses of ozone (O3), carbon monoxide (CO), nitrogen monoxide (NO), nitrogen dioxide (NO2), and the sum of nitrogen oxides (NOy). In addition, an extended set of halocarbons and a selection of VOCs (alkanes, aromatics) are measured with a time resolution of four hours since 2000 as a part of SOGE. Daily samples are taken for determination of gaseous SO2 and for particulate sulphur. The concentrations of total suspended particles are continuously observed as well as measured as 48-hour bulk samples. Measurements of methane, nitrous oxide and sulphur hexafluoride were commenced in February 2005 funded by the FOEN. Therefore, the whole set of non-CO2 greenhouse gases is now continuously monitored at the Jungfraujoch."
                    },
                    "instrument": {
                        "ob_id": 2915,
                        "uuid": "fab352335cdc4b9e9f231ebe916c8611",
                        "short_code": "instr",
                        "title": "EMPA: TEI 409C UV absorption",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11152,
                        "uuid": "84b7039a77644e048508ca384935b4ef",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from EMPA: UV absorption TEI49C at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: EMPA: UV absorption TEI49C; PLATFORMS: Jungfraujoch, Switzerland; "
                    }
                }
            ]
        },
        {
            "ob_id": 11158,
            "uuid": "e3b34f6d58b448ec8346f50d507ae619",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Met Office C-band radar at Hameldon Hill Radar Station, UK",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office C-band radar; PLATFORMS: Hameldon Hill Radar Station, UK; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3878,
                    "platform": {
                        "ob_id": 4775,
                        "uuid": "490871ffb5ee4c39b9d8cf8bbafd7b57",
                        "short_code": "plat",
                        "title": "Hameldon Hill Radar Station, UK",
                        "abstract": "Site for Met Office radar and also a link transmitter owned by CCUK. The site is located at Dunnockshaw, Lancashire, UK."
                    },
                    "instrument": {
                        "ob_id": 1003,
                        "uuid": "fe89d9092055426eb719290ce4063b88",
                        "short_code": "instr",
                        "title": "Met Office C-band radar",
                        "abstract": "UK C Band radar run by the Met Office and the Environment Agency."
                    },
                    "relatedTo": {
                        "ob_id": 11158,
                        "uuid": "e3b34f6d58b448ec8346f50d507ae619",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Met Office C-band radar at Hameldon Hill Radar Station, UK",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office C-band radar; PLATFORMS: Hameldon Hill Radar Station, UK; "
                    }
                }
            ]
        },
        {
            "ob_id": 11162,
            "uuid": "c6a1fdc1f33040f29b32f153a01611c7",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Spinning Enhanced Visible and InfraRed Imager - SEVIRI- 2 at Meteosat Second Generation 2 (MSG-2) or METEOSAT-9 for the Meteosat Second Generation (MSG) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Spinning Enhanced Visible and InfraRed Imager - SEVIRI- 2; PLATFORMS: Meteosat Second Generation 2 (MSG-2) or METEOSAT-9; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 2660,
                    "uuid": "c606cf5dba3f4a419cd95d8b4cb52b30",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Meteosat Second Generation 2 (MSG-2) or METEOSAT-9",
                    "abstract": "Mobile Platform Operation related to the: Meteosat Second Generation 2 (MSG-2) or METEOSAT-9"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3879,
                    "platform": {
                        "ob_id": 2658,
                        "uuid": "b61deca60f694b21a49daeec9489f49a",
                        "short_code": "plat",
                        "title": "Meteosat Second Generation 2 (MSG-2) or METEOSAT-9",
                        "abstract": "The second MSG was launched on 21 December 2005 on the same type of launcher as its predecessor - a standard Ariane 5 - from the same launch site - Kourou in French Guiana. It is currently in the same fixed section of orbital space as MSG-1 in geostationary orbit, close to where the equator meets the Greenwich meridian. \nThe reason for the duplication is simply to guarantee continuity of service in case of satellite failure. Weather satellites have become so crucial a part of our daily life that any long gap in service coverage has become inconceivable."
                    },
                    "instrument": {
                        "ob_id": 2659,
                        "uuid": "109f54f2aff943c2806295305d26583a",
                        "short_code": "instr",
                        "title": "Spinning Enhanced Visible and InfraRed Imager - SEVIRI- 2",
                        "abstract": "The Spinning Enhanced Visible and InfraRed Imager (SEVIRI) instrument measures in 12 spectral channels (compared to only 3 on the previous Meteosat) and records data in a 15 minute cycle (30 minutes on the previous Meteosat). The resolution of the high-resolution visible light channel measures 1 km at the sub-satellite point (compared to 2.5 km on the previous Meteosat). The second Meteosat Second Generation satellite, MSG-2, came into operational service on 21st December 2005 and was renamed Meteosat-9."
                    },
                    "relatedTo": {
                        "ob_id": 11162,
                        "uuid": "c6a1fdc1f33040f29b32f153a01611c7",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Spinning Enhanced Visible and InfraRed Imager - SEVIRI- 2 at Meteosat Second Generation 2 (MSG-2) or METEOSAT-9 for the Meteosat Second Generation (MSG) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Spinning Enhanced Visible and InfraRed Imager - SEVIRI- 2; PLATFORMS: Meteosat Second Generation 2 (MSG-2) or METEOSAT-9; "
                    }
                }
            ]
        },
        {
            "ob_id": 11166,
            "uuid": "521964214b4f4907b75ac45593f61304",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Leicester: Spectral Radiometer j(NO2) at Bukit Atur for the OP3-1 Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Leicester: Spectral Radiometer j(NO2); PLATFORMS: Bukit Atur; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3880,
                    "platform": {
                        "ob_id": 65,
                        "uuid": "ddb404d1e6114c70bac63abaad550d4e",
                        "short_code": "plat",
                        "title": "Bukit Atur",
                        "abstract": "The Bukit Atur GAW station"
                    },
                    "instrument": {
                        "ob_id": 311,
                        "uuid": "fe82ff833eaf4a9593134c237b303dc2",
                        "short_code": "instr",
                        "title": "Leicester: Spectral Radiometer j(NO2)",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11166,
                        "uuid": "521964214b4f4907b75ac45593f61304",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Leicester: Spectral Radiometer j(NO2) at Bukit Atur for the OP3-1 Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Leicester: Spectral Radiometer j(NO2); PLATFORMS: Bukit Atur; "
                    }
                }
            ]
        },
        {
            "ob_id": 11169,
            "uuid": "d6e8c641d25642b39c74e8cfaeef1fe6",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from  at Bukit Atur for the OP3-1 Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Instrument.title: DETAILS NEEDED; PLATFORMS: Bukit Atur; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3881,
                    "platform": {
                        "ob_id": 65,
                        "uuid": "ddb404d1e6114c70bac63abaad550d4e",
                        "short_code": "plat",
                        "title": "Bukit Atur",
                        "abstract": "The Bukit Atur GAW station"
                    },
                    "instrument": {
                        "ob_id": 7719,
                        "uuid": "cd8ecc9a574e4178b12ed6fae8293d9f",
                        "short_code": "instr",
                        "title": "Instrument.title: DETAILS NEEDED",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11169,
                        "uuid": "d6e8c641d25642b39c74e8cfaeef1fe6",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from  at Bukit Atur for the OP3-1 Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Instrument.title: DETAILS NEEDED; PLATFORMS: Bukit Atur; "
                    }
                }
            ]
        },
        {
            "ob_id": 11173,
            "uuid": "01abb7ef3c2248bc8bd4de92712665b1",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Salford/UFAM: Doppler Lidar at Shoeburyness, UK for the Universities Facility for Atmospheric Measurement (UFAM) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Salford/UFAM: Doppler Lidar; PLATFORMS: Shoeburyness, UK; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3882,
                    "platform": {
                        "ob_id": 1009,
                        "uuid": "f5fd392fd156428e9d4686d9c0b580fb",
                        "short_code": "plat",
                        "title": "Shoeburyness, UK",
                        "abstract": "Church End, Shoeburyness, Southend-on-Sea, Essex, UK. Field site used for trials with the Salford lidar and Salford automatic weather station in 2006."
                    },
                    "instrument": {
                        "ob_id": 1433,
                        "uuid": "46742014e0d04d798cf281be1b69c68f",
                        "short_code": "instr",
                        "title": "Salford/UFAM: Doppler Lidar",
                        "abstract": "This is a 10.6 um Doppler Lidar system for atmospheric measurements from a minimum range of 500 m-700 m up to a maximum of 9 km. This is a UFAM instrument operated by the University of Salford, UK. The instrument is a 1.55 μm eye-safe (Class 1M) scanning micro pulsed LiDAR providing profiles of aerosol backscatter coefficient (β) in units of m-1 sr-1 and radial velocity in ms-1 at user specified azimuth and elevation angles. This system has additional Doppler and depolarisation channels. A three point scanning algorithm is supplied for automated wind profile measurement: profiles of wind speed and direction can be obtained at a minimum of once every two minutes. Signal analysis, data retrievals, and data storage are performed by a PC system on-board the instrument. Users can operate the instrument remotely via the internet (not wireless) that is: users can program custom scan patterns and monitor performance. The operational software allows the user to test out head positions for a scan, level the instrument, and schedule how often the LiDAR comes out of its default operation (vertical observation or STARE Mode) to perform an operation. An internal GPS provides accurate system timing and instrument position while the extended temperature facility provides an operational temperature range of -20°C to 40°C: at temperature > 40°C this the system will automatically shutdown.\r\n\r\nThis instrument was subsequently converted into the instrument now operated by NCAS AMF as their Halo Doppler Lidar no 1."
                    },
                    "relatedTo": {
                        "ob_id": 11173,
                        "uuid": "01abb7ef3c2248bc8bd4de92712665b1",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Salford/UFAM: Doppler Lidar at Shoeburyness, UK for the Universities Facility for Atmospheric Measurement (UFAM) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Salford/UFAM: Doppler Lidar; PLATFORMS: Shoeburyness, UK; "
                    }
                }
            ]
        },
        {
            "ob_id": 11179,
            "uuid": "b3c13d922a2f43bfa2b71ad3ef2d58a8",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Leicester: Spectral Radiometer j(O1D) at Bukit Atur for the OP3-1 Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Leicester: Spectral Radiometer j(O1D); PLATFORMS: Bukit Atur; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3883,
                    "platform": {
                        "ob_id": 65,
                        "uuid": "ddb404d1e6114c70bac63abaad550d4e",
                        "short_code": "plat",
                        "title": "Bukit Atur",
                        "abstract": "The Bukit Atur GAW station"
                    },
                    "instrument": {
                        "ob_id": 315,
                        "uuid": "6e6a11c756bf49e48dca59ca002f351b",
                        "short_code": "instr",
                        "title": "Leicester: Spectral Radiometer j(O1D)",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11179,
                        "uuid": "b3c13d922a2f43bfa2b71ad3ef2d58a8",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Leicester: Spectral Radiometer j(O1D) at Bukit Atur for the OP3-1 Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Leicester: Spectral Radiometer j(O1D); PLATFORMS: Bukit Atur; "
                    }
                }
            ]
        },
        {
            "ob_id": 11183,
            "uuid": "e1c7536269704f2f96f1e43c62e8a6d0",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Automatic Weather Station (AWS) at MIDAS Global weather stations for the Met Office",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Automatic Weather Station (AWS); PLATFORMS: MIDAS Global weather stations; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3884,
                    "platform": {
                        "ob_id": 11182,
                        "uuid": "208cd99813da4094ae90e4cf3faadf7c",
                        "short_code": "plat",
                        "title": "MIDAS Global weather stations",
                        "abstract": "Global weather stations in MIDAS, including stations in Africa, Europe, Antarctica, North, Central, and South America, Asia, and South-west Pacific."
                    },
                    "instrument": {
                        "ob_id": 1061,
                        "uuid": "a2f40afd5f054601a037d48a9aac17e9",
                        "short_code": "instr",
                        "title": "Automatic Weather Station (AWS)",
                        "abstract": "An automatic weather station (AWS) is an automated version of the traditional weather station, either to save human labour or to enable measurements from remote areas. The system may report in near real time via ARGOS and the Global telecommunications system, or save the data for later recovery."
                    },
                    "relatedTo": {
                        "ob_id": 11183,
                        "uuid": "e1c7536269704f2f96f1e43c62e8a6d0",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Automatic Weather Station (AWS) at MIDAS Global weather stations for the Met Office",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Automatic Weather Station (AWS); PLATFORMS: MIDAS Global weather stations; "
                    }
                }
            ]
        },
        {
            "ob_id": 11186,
            "uuid": "19d52c5af1444a649d9739ba5e904edc",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from FAAM/BAE systems: Reduced Vertical Separation Minimum system (used on turbulence probe) for the Joint Airborne IASI Validation Experiment (JAIVEX) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: FAAM/BAE systems: Reduced Vertical Separation Minimum system (used on turbulence probe); ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": []
        },
        {
            "ob_id": 11189,
            "uuid": "388a4c82d1ec43a99333cded6a5d3112",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Manchester/UFAM: Differential Mobility Particle Sizer - formerly umist-dmps at Bukit Atur for the Aerosol Coupling in the Earth System (ACES) Project , Part of the APPRAISE (Aerosol Properties, PRocesses And Influences on the Earth's climate) Program Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Manchester/UFAM: Differential Mobility Particle Sizer - formerly umist-dmps; PLATFORMS: Bukit Atur; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3886,
                    "platform": {
                        "ob_id": 65,
                        "uuid": "ddb404d1e6114c70bac63abaad550d4e",
                        "short_code": "plat",
                        "title": "Bukit Atur",
                        "abstract": "The Bukit Atur GAW station"
                    },
                    "instrument": {
                        "ob_id": 223,
                        "uuid": "fcbdb31c451e49509ab6c438ac139098",
                        "short_code": "instr",
                        "title": "Manchester/UFAM: Differential Mobility Particle Sizer - formerly umist-dmps",
                        "abstract": "A Differential Mobility Particle Sizer (DMPS) operated by the University of Manchester which measures aerosol size distribution.  The DMPS classifies particles according to electrical mobility in a differential mobility analyser and counts particles of given mobility using a condensation particle counter. The Manchester DMPS uses two such DMA’s and CPC of different specifications to measure aerosol size distributions from 3.5 – 800nm, with a complete scan taking ten minutes."
                    },
                    "relatedTo": {
                        "ob_id": 11189,
                        "uuid": "388a4c82d1ec43a99333cded6a5d3112",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Manchester/UFAM: Differential Mobility Particle Sizer - formerly umist-dmps at Bukit Atur for the Aerosol Coupling in the Earth System (ACES) Project , Part of the APPRAISE (Aerosol Properties, PRocesses And Influences on the Earth's climate) Program Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Manchester/UFAM: Differential Mobility Particle Sizer - formerly umist-dmps; PLATFORMS: Bukit Atur; "
                    }
                }
            ]
        },
        {
            "ob_id": 11193,
            "uuid": "2267d7441933472784765698f15eb481",
            "short_code": "acq",
            "title": "Acquisition Process for: AVHRR/3 data on NOAA-15 for 1999-2001",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Advanced Very High Resolution Radiometer 3 (AVHRR/3); PLATFORMS: NOAA-15; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 1818,
                    "uuid": "85413707bcd94206945140485a57789f",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: NOAA-15",
                    "abstract": "Mobile Platform Operation related to the: NOAA-15"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3887,
                    "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": 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": 11193,
                        "uuid": "2267d7441933472784765698f15eb481",
                        "short_code": "acq",
                        "title": "Acquisition Process for: AVHRR/3 data on NOAA-15 for 1999-2001",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Advanced Very High Resolution Radiometer 3 (AVHRR/3); PLATFORMS: NOAA-15; "
                    }
                }
            ]
        },
        {
            "ob_id": 11200,
            "uuid": "d92b7b2696f442988180229238ce4e2e",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Met Office - Telemetered tipping bucket raingauges at Coney Green, UK for the Natural Environment Research Council (NERC)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office - Telemetered tipping bucket raingauges; PLATFORMS: Coney Green, UK; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3888,
                    "platform": {
                        "ob_id": 7484,
                        "uuid": "ed38bc524b404d90bdae86d424bf66bc",
                        "short_code": "plat",
                        "title": "Coney Green, UK",
                        "abstract": "Raingauge \r\nNational Grid reference 3787 4075"
                    },
                    "instrument": {
                        "ob_id": 6458,
                        "uuid": "25003d5874064f929dbf14708dee4db4",
                        "short_code": "instr",
                        "title": "Met Office - Telemetered tipping bucket raingauges",
                        "abstract": "The tipping bucket raingauge is particularly suitable for the automation of rainfall measurement"
                    },
                    "relatedTo": {
                        "ob_id": 11200,
                        "uuid": "d92b7b2696f442988180229238ce4e2e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Met Office - Telemetered tipping bucket raingauges at Coney Green, UK for the Natural Environment Research Council (NERC)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office - Telemetered tipping bucket raingauges; PLATFORMS: Coney Green, UK; "
                    }
                }
            ]
        },
        {
            "ob_id": 11203,
            "uuid": "f96d29fa3c5649c2adba4e92902c0e2f",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Mid-tide bubbler gauge at GLOSS station network",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Mid-tide bubbler gauge; PLATFORMS: GLOSS station network; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3889,
                    "platform": {
                        "ob_id": 6622,
                        "uuid": "ce0040e923c04c90b75c12cab962d27f",
                        "short_code": "plat",
                        "title": "GLOSS station network",
                        "abstract": "The main component of GLOSS is the 'Global Core Network' (GCN) of 290 sea level stations around the world for long term climate change and oceanographic sea level monitoring."
                    },
                    "instrument": {
                        "ob_id": 6627,
                        "uuid": "389aadd447254e87afbecc3e37e6964f",
                        "short_code": "instr",
                        "title": "Mid-tide bubbler gauge",
                        "abstract": "Type of tide gauge to measure sea levels."
                    },
                    "relatedTo": {
                        "ob_id": 11203,
                        "uuid": "f96d29fa3c5649c2adba4e92902c0e2f",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Mid-tide bubbler gauge at GLOSS station network",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Mid-tide bubbler gauge; PLATFORMS: GLOSS station network; "
                    }
                }
            ]
        },
        {
            "ob_id": 11206,
            "uuid": "fc6102f6b62b466b925d40873bfc45b6",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Munro float gauge at GLOSS station network",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Munro float gauge; PLATFORMS: GLOSS station network; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3890,
                    "platform": {
                        "ob_id": 6622,
                        "uuid": "ce0040e923c04c90b75c12cab962d27f",
                        "short_code": "plat",
                        "title": "GLOSS station network",
                        "abstract": "The main component of GLOSS is the 'Global Core Network' (GCN) of 290 sea level stations around the world for long term climate change and oceanographic sea level monitoring."
                    },
                    "instrument": {
                        "ob_id": 6631,
                        "uuid": "82aad8c0aeb34cfa8b31421db9baf3b8",
                        "short_code": "instr",
                        "title": "Munro float gauge",
                        "abstract": "Type of tide gauge to measure sea levels."
                    },
                    "relatedTo": {
                        "ob_id": 11206,
                        "uuid": "fc6102f6b62b466b925d40873bfc45b6",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Munro float gauge at GLOSS station network",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Munro float gauge; PLATFORMS: GLOSS station network; "
                    }
                }
            ]
        },
        {
            "ob_id": 11209,
            "uuid": "8c66fe3133be40ef9b50360585c144aa",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Met Office: Microwave Airborne Radiometer Scanning System (MARSS) at FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE for the Facility for Airborne Atmospheric Measurements (FAAM) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office: Microwave Airborne Radiometer Scanning System (MARSS); PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 53,
                    "uuid": "d7eea365352547a18b58f128b34099f3",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                    "abstract": "Mobile Platform Operation related to the: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 5288,
                    "platform": {
                        "ob_id": 51,
                        "uuid": "dda4596d5d374564acf8c79b7a119127",
                        "short_code": "plat",
                        "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                        "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
                    },
                    "instrument": {
                        "ob_id": 2864,
                        "uuid": "b0a893d0b4ab4f55951aa53b2ff82f11",
                        "short_code": "instr",
                        "title": "Met Office: Microwave Airborne Radiometer Scanning System (MARSS)",
                        "abstract": "MARSS (Microwave Airborne Radiometer Scanning System) is an along-track scanning, total power microwave radiometer which measures in five channels, two window channels at 89 and 157 GHz and three channels centred on the water vapour absorption line at 183.31 GHz."
                    },
                    "relatedTo": {
                        "ob_id": 11209,
                        "uuid": "8c66fe3133be40ef9b50360585c144aa",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Met Office: Microwave Airborne Radiometer Scanning System (MARSS) at FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE for the Facility for Airborne Atmospheric Measurements (FAAM) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office: Microwave Airborne Radiometer Scanning System (MARSS); PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; "
                    }
                }
            ]
        },
        {
            "ob_id": 11214,
            "uuid": "17573854514c4a209c869b69c01c96d6",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from FAAM/BAE systems: TECO 49 UV photometric ozone instrument for the Joint Airborne IASI Validation Experiment (JAIVEX) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: FAAM/BAE systems: TECO 49 UV photometric ozone instrument; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": []
        },
        {
            "ob_id": 11217,
            "uuid": "be857fcecb204becbe17b12497d8dd89",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from UEA: GC mass spec at Mace Head Research Facility, Ireland for the ACSOE - MAGE Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UEA: GC mass spec; PLATFORMS: Mace Head Research Facility, Ireland; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 4804,
                    "platform": {
                        "ob_id": 1924,
                        "uuid": "409b3e2004154837805552cb3cb7a546",
                        "short_code": "plat",
                        "title": "Mace Head Atmospheric Research Facility, Ireland",
                        "abstract": "The Mace Head Atmospheric Research Facility is located in Carna, County Galway, Ireland and is managed by the Department of Experimental Physics, Atmospheric Science Group, National University of Ireland, Galway. It has the dual status of a WMO GAW research and monitoring 'global' station and an EMEP supersite. It has the stations ID \"MHD'"
                    },
                    "instrument": {
                        "ob_id": 192,
                        "uuid": "55d834d4c2d8462b836f53af8ba10efe",
                        "short_code": "instr",
                        "title": "UEA: Gas Chromatograph with Mass Spectrometer (GC MS)",
                        "abstract": "University of East Anglia Gas Chromatograph Mass Spectrometer (GC MS)"
                    },
                    "relatedTo": {
                        "ob_id": 11217,
                        "uuid": "be857fcecb204becbe17b12497d8dd89",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from UEA: GC mass spec at Mace Head Research Facility, Ireland for the ACSOE - MAGE Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UEA: GC mass spec; PLATFORMS: Mace Head Research Facility, Ireland; "
                    }
                }
            ]
        },
        {
            "ob_id": 11220,
            "uuid": "3da4c99460a1437884ae0acd051ba4d8",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Dunkeswell: Met Office Windprofiler 1290MHz 1 at Global Radiosonde Network",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Dunkeswell: Met Office Windprofiler 1290MHz 1; PLATFORMS: Global Radiosonde Network; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3894,
                    "platform": {
                        "ob_id": 5504,
                        "uuid": "181b47abb3314f6a94e8938e3b83be28",
                        "short_code": "plat",
                        "title": "Global Radiosonde Network",
                        "abstract": "Platform.abstract: DETAILS NEEDED"
                    },
                    "instrument": {
                        "ob_id": 1022,
                        "uuid": "dcc2c0244c144137919eecf8db8a6baf",
                        "short_code": "instr",
                        "title": "Dunkeswell: Met Office Windprofiler 1290MHz 1",
                        "abstract": "The Dunkeswell Radian LAP3000 is permanently located at an existing SAMOS site within Dunkeswell Airfield.  The Dunkeswell profiler was one of two Radian 1290MHz profilers installed in the UK in February 1999. This system is an integral part of the UK operational upper air network. Dunkeswell, like the other sites, is configured to operate in two modes. The low mode provides high resolution wind information up to 2km above the surface, while the high mode, with 210m resolution can see up to 8km under appropriate conditions"
                    },
                    "relatedTo": {
                        "ob_id": 11220,
                        "uuid": "3da4c99460a1437884ae0acd051ba4d8",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Dunkeswell: Met Office Windprofiler 1290MHz 1 at Global Radiosonde Network",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Dunkeswell: Met Office Windprofiler 1290MHz 1; PLATFORMS: Global Radiosonde Network; "
                    }
                }
            ]
        },
        {
            "ob_id": 11223,
            "uuid": "59a0b706899a4043b89b72f38f1c2904",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from UEA: Crannox NOx, O3, NOy at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UEA: Crannox NOx, O3, NOy; PLATFORMS: Jungfraujoch, Switzerland; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3895,
                    "platform": {
                        "ob_id": 1523,
                        "uuid": "97bdfb9741f441eebfb16440ebbb0f92",
                        "short_code": "plat",
                        "title": "Jungfraujoch Research Station",
                        "abstract": "The high altitude research station Jungfraujoch (7° 59' E, 46° 32' N, 3580 m a.s.l.) is situated on a mountain saddle in the central Swiss Alps between the Jungfrau (4158 m a.s.l.) in the West and the Moench (4099 m a.s.l.) in the East. The International Foundation High Altitude Research Stations Jungfraujoch and Gornergrat (HFSJG) runs the research station and provides the infrastructure and support for scientific research. Due to its unique place, the year-round accessibility, and the excellent infrastructure, the Jungfraujoch research station is well suited for long-term ground-based monitoring of trace gas concentrations trends in the free troposphere. Due to its location in central Europe and its proximity to anthropogenic greenhouse gas source regions it is also an appropriate study site for European regional source allocations during pollution events. The research activities of EMPA at the Jungfraujoch are conducted within the scope of the Swiss National Air Pollution Monitoring Network (NABEL) funded by the Swiss Federal Office for the Environment (FOEN) and the Global Atmosphere Watch Program (GAW) of the World Meteorological Organization (WMO). The measurement programme at Jungfraujoch includes continuous in-situ analyses of ozone (O3), carbon monoxide (CO), nitrogen monoxide (NO), nitrogen dioxide (NO2), and the sum of nitrogen oxides (NOy). In addition, an extended set of halocarbons and a selection of VOCs (alkanes, aromatics) are measured with a time resolution of four hours since 2000 as a part of SOGE. Daily samples are taken for determination of gaseous SO2 and for particulate sulphur. The concentrations of total suspended particles are continuously observed as well as measured as 48-hour bulk samples. Measurements of methane, nitrous oxide and sulphur hexafluoride were commenced in February 2005 funded by the FOEN. Therefore, the whole set of non-CO2 greenhouse gases is now continuously monitored at the Jungfraujoch."
                    },
                    "instrument": {
                        "ob_id": 1928,
                        "uuid": "ec9859718cb84f699f7a3181dfa5d24b",
                        "short_code": "instr",
                        "title": "UEA: CRANOX NOx, O3, NOy",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11223,
                        "uuid": "59a0b706899a4043b89b72f38f1c2904",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from UEA: Crannox NOx, O3, NOy at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UEA: Crannox NOx, O3, NOy; PLATFORMS: Jungfraujoch, Switzerland; "
                    }
                }
            ]
        },
        {
            "ob_id": 11227,
            "uuid": "8d8eb2329fb94e568928a26ac1f5b8c7",
            "short_code": "acq",
            "title": "Acquisition Process for: Radiosonde anomalies from the HadAT radiosonde network (1958-present)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Radiosonde; PLATFORMS: HadAT radiosonde network; \r\n\r\nThe radiosonde network used to produce these data are derived from 676 individual radiosonde stations with long-term records. Because of the criteria of data longevity the resulting dataset is limited to land areas and primarily Northern Hemisphere locations. Radiosondes are single launch instruments and there have been many changes in instruments and observing practices with time. HadAT has used a neighbour-based approach to attempt to adjust for these effects and produce a homogeneous product suitable for climate applications.",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3896,
                    "platform": {
                        "ob_id": 11226,
                        "uuid": "215557b822834f8c86b935e45274358f",
                        "short_code": "plat",
                        "title": "HadAT radiosonde network",
                        "abstract": "Set of global radiosonde stations used to compile the HadAT dataset."
                    },
                    "instrument": {
                        "ob_id": 912,
                        "uuid": "e0c08343c2a74974a912ccb96f514130",
                        "short_code": "instr",
                        "title": "Radiosonde",
                        "abstract": "The radiosonde is a lightweight, balloon-borne instrument that measures profiles of pressure, temperature and humidity from the ground to approximately 40km.The radiosonde is equipped with a radio transmitter for sending the measurements to the observing station."
                    },
                    "relatedTo": {
                        "ob_id": 11227,
                        "uuid": "8d8eb2329fb94e568928a26ac1f5b8c7",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Radiosonde anomalies from the HadAT radiosonde network (1958-present)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Radiosonde; PLATFORMS: HadAT radiosonde network; \r\n\r\nThe radiosonde network used to produce these data are derived from 676 individual radiosonde stations with long-term records. Because of the criteria of data longevity the resulting dataset is limited to land areas and primarily Northern Hemisphere locations. Radiosondes are single launch instruments and there have been many changes in instruments and observing practices with time. HadAT has used a neighbour-based approach to attempt to adjust for these effects and produce a homogeneous product suitable for climate applications."
                    }
                }
            ]
        },
        {
            "ob_id": 11231,
            "uuid": "5fff9e7433a14f0ba98c0b7d2178dd4b",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Manchester: Single Particle Soot Photometer (ST2) at FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE for the ADIENT (Appraising the Direct Impacts of aErosol oN climaTe) project, Part of the APPRAISE (Aerosol Properties, PRocesses And Influences on the Earth's climate) Program Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Manchester: Single Particle Soot Photometer (ST2); PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 53,
                    "uuid": "d7eea365352547a18b58f128b34099f3",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                    "abstract": "Mobile Platform Operation related to the: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3897,
                    "platform": {
                        "ob_id": 51,
                        "uuid": "dda4596d5d374564acf8c79b7a119127",
                        "short_code": "plat",
                        "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                        "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
                    },
                    "instrument": {
                        "ob_id": 11230,
                        "uuid": "4475880cd0f2432fa88d2cbe1e03a791",
                        "short_code": "instr",
                        "title": "Manchester: Single Particle Soot Photometer (SP2)",
                        "abstract": "The Single Particle Soot Photometer (SP2) is manufactured by Droplet Measurement Technologies (DMT). It measures the soot (also known as black carbon) content of individual airborne particles, known as aerosols. \r\n\r\nThe SP2 is a laser-based instrument, which detects black carbon particles by heating them to their point of 'incandescence'. This results in the emission of radiation that can be measured and related to the mass of black carbon. \r\n\r\nThe instrument can be operated in a range of environments (lab, ground-based, aircraft) and its high sensitivity and fast response makes it ideal for a number of atmospheric science applications. The measurement frequency of this instrument is 1Hz. \r\n\r\nThe outputs include: black carbon mass, number and size; as well as information relating to the mixing state of black carbon-containing particles. Number and volume concentration of scattering particles; as well as their optical size are also included. \r\n\r\nBlack carbon is an important component of atmospheric aerosol and is a strong absorber of solar radiation. It is a product of incomplete combustion activities and the major sources include vehicle engines, burning of domestic fuels for heating/cooking and forest/agricultural fires. Human activities have increased the amount of black carbon in the atmosphere, which leads to a warming of the Earth's temperature.\r\n\r\nThis instrument is regularly used on the FAAM BAe 146 aircraft."
                    },
                    "relatedTo": {
                        "ob_id": 11231,
                        "uuid": "5fff9e7433a14f0ba98c0b7d2178dd4b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Manchester: Single Particle Soot Photometer (ST2) at FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE for the ADIENT (Appraising the Direct Impacts of aErosol oN climaTe) project, Part of the APPRAISE (Aerosol Properties, PRocesses And Influences on the Earth's climate) Program Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Manchester: Single Particle Soot Photometer (ST2); PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; "
                    }
                }
            ]
        },
        {
            "ob_id": 11240,
            "uuid": "c2e4821979e34ff7b5842c4a33af759b",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from FAAM/BAE systems: Particle Soot Absorption Photometer (PSAP aka SOOTY) for the Joint Airborne IASI Validation Experiment (JAIVEX) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: FAAM/BAE systems: Particle Soot Absorption Photometer (PSAP aka SOOTY); ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": []
        },
        {
            "ob_id": 11243,
            "uuid": "0f999987f77346f9b39a5761379464df",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Automatic Weather Station (AWS) at Armagh Observatory, Northern Ireland, UK for the Armagh Observatory, UK Collection",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Automatic Weather Station (AWS); PLATFORMS: Armagh Observatory, Northern Ireland, UK; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3899,
                    "platform": {
                        "ob_id": 2319,
                        "uuid": "12a6c6f652ba42bdbde7d5be321127aa",
                        "short_code": "plat",
                        "title": "Armagh Observatory, Northern Ireland, UK",
                        "abstract": "The Armagh Observatory is a modern astronomical research institute with a rich heritage. Founded in 1790 by Archbishop Richard Robinson, the Observatory is one of the UK and Ireland's leading scientific research establishments. Around 25 astronomers are actively studying Stellar Astrophysics, the Sun, Solar System astronomy, and the Earth's climate."
                    },
                    "instrument": {
                        "ob_id": 1061,
                        "uuid": "a2f40afd5f054601a037d48a9aac17e9",
                        "short_code": "instr",
                        "title": "Automatic Weather Station (AWS)",
                        "abstract": "An automatic weather station (AWS) is an automated version of the traditional weather station, either to save human labour or to enable measurements from remote areas. The system may report in near real time via ARGOS and the Global telecommunications system, or save the data for later recovery."
                    },
                    "relatedTo": {
                        "ob_id": 11243,
                        "uuid": "0f999987f77346f9b39a5761379464df",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Automatic Weather Station (AWS) at Armagh Observatory, Northern Ireland, UK for the Armagh Observatory, UK Collection",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Automatic Weather Station (AWS); PLATFORMS: Armagh Observatory, Northern Ireland, UK; "
                    }
                }
            ]
        },
        {
            "ob_id": 11246,
            "uuid": "6b3f3d7f666a41f6a3e72cbb81862d8e",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from EMPA: ND-IR Horiba ARMA 360 at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: EMPA: ND-IR Horiba ARMA 360; PLATFORMS: Jungfraujoch, Switzerland; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3900,
                    "platform": {
                        "ob_id": 1523,
                        "uuid": "97bdfb9741f441eebfb16440ebbb0f92",
                        "short_code": "plat",
                        "title": "Jungfraujoch Research Station",
                        "abstract": "The high altitude research station Jungfraujoch (7° 59' E, 46° 32' N, 3580 m a.s.l.) is situated on a mountain saddle in the central Swiss Alps between the Jungfrau (4158 m a.s.l.) in the West and the Moench (4099 m a.s.l.) in the East. The International Foundation High Altitude Research Stations Jungfraujoch and Gornergrat (HFSJG) runs the research station and provides the infrastructure and support for scientific research. Due to its unique place, the year-round accessibility, and the excellent infrastructure, the Jungfraujoch research station is well suited for long-term ground-based monitoring of trace gas concentrations trends in the free troposphere. Due to its location in central Europe and its proximity to anthropogenic greenhouse gas source regions it is also an appropriate study site for European regional source allocations during pollution events. The research activities of EMPA at the Jungfraujoch are conducted within the scope of the Swiss National Air Pollution Monitoring Network (NABEL) funded by the Swiss Federal Office for the Environment (FOEN) and the Global Atmosphere Watch Program (GAW) of the World Meteorological Organization (WMO). The measurement programme at Jungfraujoch includes continuous in-situ analyses of ozone (O3), carbon monoxide (CO), nitrogen monoxide (NO), nitrogen dioxide (NO2), and the sum of nitrogen oxides (NOy). In addition, an extended set of halocarbons and a selection of VOCs (alkanes, aromatics) are measured with a time resolution of four hours since 2000 as a part of SOGE. Daily samples are taken for determination of gaseous SO2 and for particulate sulphur. The concentrations of total suspended particles are continuously observed as well as measured as 48-hour bulk samples. Measurements of methane, nitrous oxide and sulphur hexafluoride were commenced in February 2005 funded by the FOEN. Therefore, the whole set of non-CO2 greenhouse gases is now continuously monitored at the Jungfraujoch."
                    },
                    "instrument": {
                        "ob_id": 2916,
                        "uuid": "8f12f092b1d14fc8861dcc95d7e440d3",
                        "short_code": "instr",
                        "title": "EMPA: Horiba Arma-360 (ND-IR technique)",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11246,
                        "uuid": "6b3f3d7f666a41f6a3e72cbb81862d8e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from EMPA: ND-IR Horiba ARMA 360 at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: EMPA: ND-IR Horiba ARMA 360; PLATFORMS: Jungfraujoch, Switzerland; "
                    }
                }
            ]
        },
        {
            "ob_id": 11249,
            "uuid": "bfd322a0ce1f457183d80a3f3279dc13",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Met Office: Airborne Research Interferometer Evaluation System (ARIES) at FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE for the Facility for Airborne Atmospheric Measurements (FAAM) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office: Airborne Research Interferometer Evaluation System (ARIES); PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 53,
                    "uuid": "d7eea365352547a18b58f128b34099f3",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                    "abstract": "Mobile Platform Operation related to the: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 5289,
                    "platform": {
                        "ob_id": 51,
                        "uuid": "dda4596d5d374564acf8c79b7a119127",
                        "short_code": "plat",
                        "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                        "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
                    },
                    "instrument": {
                        "ob_id": 448,
                        "uuid": "a7e69cf336ab4cd985bb4a03508c834d",
                        "short_code": "instr",
                        "title": "Met Office: Airborne Research Interferometer Evaluation System (ARIES)",
                        "abstract": "ARIES is a Fourier transform spectrometer based on the Bomem MB100 interferometer, modified by ABB Bomem (Canada) for airborne use, with Met Office designed pointing optics, external black bodies and control electronics. Although designed, and primarily used, for airborne measurements ARIES can also be used for ground based work away from the aircraft."
                    },
                    "relatedTo": {
                        "ob_id": 11249,
                        "uuid": "bfd322a0ce1f457183d80a3f3279dc13",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Met Office: Airborne Research Interferometer Evaluation System (ARIES) at FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE for the Facility for Airborne Atmospheric Measurements (FAAM) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office: Airborne Research Interferometer Evaluation System (ARIES); PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; "
                    }
                }
            ]
        },
        {
            "ob_id": 11255,
            "uuid": "8768b255087f42bd8c5dbadf9c2ffd2d",
            "short_code": "acq",
            "title": "Acquisition Process for: Temperature sensors from an unknown set of Met Office UK stations from 1659 to 31 Dec. 1973 (deployment_64)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office station temperature sensor; PLATFORMS: partially unknown set of UK CET stations; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3902,
                    "platform": {
                        "ob_id": 32,
                        "uuid": "a06054a34a6f4a72a87e3390a8136492",
                        "short_code": "plat",
                        "title": "partially unknown set of UK CET stations",
                        "abstract": "Partially unknown set of stations used by Manley, in the triangular area between Preston, Bristol and London to produce monthly series of Central England Temperature. Some of the stations known to have been used were: London, Lyndon Hall, Rutland and Oxford (Radcliffe Observatory)."
                    },
                    "instrument": {
                        "ob_id": 39,
                        "uuid": "33a6cbd8e65b4c679803244f4bf66707",
                        "short_code": "instr",
                        "title": "Met Office station temperature sensor",
                        "abstract": "Temperature sensor installed and used to monitor air temperature at stations on the Met Office network."
                    },
                    "relatedTo": {
                        "ob_id": 11255,
                        "uuid": "8768b255087f42bd8c5dbadf9c2ffd2d",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Temperature sensors from an unknown set of Met Office UK stations from 1659 to 31 Dec. 1973 (deployment_64)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office station temperature sensor; PLATFORMS: partially unknown set of UK CET stations; "
                    }
                }
            ]
        },
        {
            "ob_id": 11259,
            "uuid": "b33fb85bf8e94af6b0083986eabc928f",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from GC-ECD at Southern Surveyor research vessel for the Southern Ocean Atmospheric Photochemistry Experiment 2 (SOAPEX-2) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: GC-ECD; PLATFORMS: Southern Surveyor research vessel; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 3975,
                    "uuid": "e9986ce3bbdc4286972097519961fb06",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Southern Surveyor research vessel",
                    "abstract": "Mobile Platform Operation related to the: Southern Surveyor research vessel"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3903,
                    "platform": {
                        "ob_id": 3974,
                        "uuid": "2760866d3e774b2ab9f7896b9c831dd3",
                        "short_code": "plat",
                        "title": "Southern Surveyor research vessel",
                        "abstract": "Research vessel operated by CSIRO, Australia."
                    },
                    "instrument": {
                        "ob_id": 11258,
                        "uuid": "c1110ce2f38949a3867f8d2dcf0d6047",
                        "short_code": "instr",
                        "title": "GC-ECD",
                        "abstract": "Gas Chrmoatography (GC) - Electrolytic Conductivity Detection (ECD)"
                    },
                    "relatedTo": {
                        "ob_id": 11259,
                        "uuid": "b33fb85bf8e94af6b0083986eabc928f",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from GC-ECD at Southern Surveyor research vessel for the Southern Ocean Atmospheric Photochemistry Experiment 2 (SOAPEX-2) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: GC-ECD; PLATFORMS: Southern Surveyor research vessel; "
                    }
                }
            ]
        },
        {
            "ob_id": 11262,
            "uuid": "76081e922d5b47ec9f324ef7f1ee4207",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from FAAM/BAE systems: Liquid Water Content Probe (Johnson-Williams) for the Joint Airborne IASI Validation Experiment (JAIVEX) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: FAAM/BAE systems: Liquid Water Content Probe (Johnson-Williams); ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": []
        },
        {
            "ob_id": 11265,
            "uuid": "9613a77c09a94c049c4ffdae04226fcd",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from UEA: Packed column GC-ECD at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UEA: Packed column GC-ECD; PLATFORMS: Jungfraujoch, Switzerland; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3905,
                    "platform": {
                        "ob_id": 1523,
                        "uuid": "97bdfb9741f441eebfb16440ebbb0f92",
                        "short_code": "plat",
                        "title": "Jungfraujoch Research Station",
                        "abstract": "The high altitude research station Jungfraujoch (7° 59' E, 46° 32' N, 3580 m a.s.l.) is situated on a mountain saddle in the central Swiss Alps between the Jungfrau (4158 m a.s.l.) in the West and the Moench (4099 m a.s.l.) in the East. The International Foundation High Altitude Research Stations Jungfraujoch and Gornergrat (HFSJG) runs the research station and provides the infrastructure and support for scientific research. Due to its unique place, the year-round accessibility, and the excellent infrastructure, the Jungfraujoch research station is well suited for long-term ground-based monitoring of trace gas concentrations trends in the free troposphere. Due to its location in central Europe and its proximity to anthropogenic greenhouse gas source regions it is also an appropriate study site for European regional source allocations during pollution events. The research activities of EMPA at the Jungfraujoch are conducted within the scope of the Swiss National Air Pollution Monitoring Network (NABEL) funded by the Swiss Federal Office for the Environment (FOEN) and the Global Atmosphere Watch Program (GAW) of the World Meteorological Organization (WMO). The measurement programme at Jungfraujoch includes continuous in-situ analyses of ozone (O3), carbon monoxide (CO), nitrogen monoxide (NO), nitrogen dioxide (NO2), and the sum of nitrogen oxides (NOy). In addition, an extended set of halocarbons and a selection of VOCs (alkanes, aromatics) are measured with a time resolution of four hours since 2000 as a part of SOGE. Daily samples are taken for determination of gaseous SO2 and for particulate sulphur. The concentrations of total suspended particles are continuously observed as well as measured as 48-hour bulk samples. Measurements of methane, nitrous oxide and sulphur hexafluoride were commenced in February 2005 funded by the FOEN. Therefore, the whole set of non-CO2 greenhouse gases is now continuously monitored at the Jungfraujoch."
                    },
                    "instrument": {
                        "ob_id": 2921,
                        "uuid": "d40506b4be3b4309af3235282eb03391",
                        "short_code": "instr",
                        "title": "UEA: Packed column GC-ECD",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11265,
                        "uuid": "9613a77c09a94c049c4ffdae04226fcd",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from UEA: Packed column GC-ECD at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UEA: Packed column GC-ECD; PLATFORMS: Jungfraujoch, Switzerland; "
                    }
                }
            ]
        },
        {
            "ob_id": 11274,
            "uuid": "419e5afec3be48b09ac04dd3bb65a185",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Manchester/UFAM: Aerosol Mass Spectrometer (AMS) - formerly umist-ams at FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE for the ADIENT (Appraising the Direct Impacts of aErosol oN climaTe) project, Part of the APPRAISE (Aerosol Properties, PRocesses And Influences on the Earth's climate) Program Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Manchester/UFAM: Aerosol Mass Spectrometer (AMS) - formerly umist-ams; PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 53,
                    "uuid": "d7eea365352547a18b58f128b34099f3",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                    "abstract": "Mobile Platform Operation related to the: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3907,
                    "platform": {
                        "ob_id": 51,
                        "uuid": "dda4596d5d374564acf8c79b7a119127",
                        "short_code": "plat",
                        "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                        "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
                    },
                    "instrument": {
                        "ob_id": 99,
                        "uuid": "98ab5fc9e63c403792e90e6b9b69e3c8",
                        "short_code": "instr",
                        "title": "University of Manchester/UFAM: Aerosol Mass Spectrometer (AMS) - formerly umist-ams",
                        "abstract": "The Aerodyne aerosol mass spectrometer (AMS) is the only currently available instrument capable of providing quantitative size and chemical mass loading information in real-time for non-refractory sub-micron aerosol particles. The AMS couples size-resolved particle sampling and mass spectrometric techniques into a single real-time measurement system. The Aerodyne AMS has been deployed world-wide at fixed sites, and on mobile laboratory, ship and aircraft platforms. Over 100 instruments are in use in industrial, academic and government laboratories.\r\n\r\nScientifically, the instrument can deliver quantitative mass concentrations of the major non-refractory chemical species present in submicron particles (ammonium, nitrate, sulphate, organics and non-sea-salt chloride) in microgrammes per cubic metre. It is also capable of delivering these concentrations as a function of diameter as a dM/dlog(D) distribution. Further to this, information on the chemical nature of the organic fraction can be derived by inspecting the relative sizes of the peaks within the mass spectrum. In order to produce fully quality assured and meaningful results, the data must be processed offline or near-real-time. The Compact Time-of-Flight AMS (C-ToF-AMS) is a version that enables continuous acquisition of complete mass spectra (1-800 m/z) of all sampled particles at rates as fast as 80 kHz."
                    },
                    "relatedTo": {
                        "ob_id": 11274,
                        "uuid": "419e5afec3be48b09ac04dd3bb65a185",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Manchester/UFAM: Aerosol Mass Spectrometer (AMS) - formerly umist-ams at FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE for the ADIENT (Appraising the Direct Impacts of aErosol oN climaTe) project, Part of the APPRAISE (Aerosol Properties, PRocesses And Influences on the Earth's climate) Program Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Manchester/UFAM: Aerosol Mass Spectrometer (AMS) - formerly umist-ams; PLATFORMS: FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE; "
                    }
                }
            ]
        },
        {
            "ob_id": 11277,
            "uuid": "fe1eac4083db49419f3460f3bf828e99",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Spinning Enhanced Visible and InfraRed Imager - SEVIRI-1 at Meteosat Second Generation 1  (MSG-1) or METEOSAT-8 for the Meteosat Second Generation (MSG) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Spinning Enhanced Visible and InfraRed Imager - SEVIRI-1; PLATFORMS: Meteosat Second Generation 1  (MSG-1) or METEOSAT-8; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 2652,
                    "uuid": "de30db0db31144b087ad0d4ddc5b02ca",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Meteosat Second Generation 1  (MSG-1) or METEOSAT-8",
                    "abstract": "Mobile Platform Operation related to the: Meteosat Second Generation 1  (MSG-1) or METEOSAT-8"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3908,
                    "platform": {
                        "ob_id": 2650,
                        "uuid": "07ef82cad2ec4bc79efb7ba41b7043df",
                        "short_code": "plat",
                        "title": "Meteosat Second Generation 1  (MSG-1) or METEOSAT-8",
                        "abstract": "Launched on 28 August 2002, the first Meteosat Second Generation (MSG) satellite became operational on 29 January 2004, when it was redesignated Meteosat-8. Since then it has continuously returned highly detailed imagery of Europe, the North Atlantic and Africa every 15 minutes, for operational use by meteorologists.\n MSG-1 has a nominal lifetime of seven years."
                    },
                    "instrument": {
                        "ob_id": 2651,
                        "uuid": "f16d9f9f95db42b0a1db527ef62c9fdd",
                        "short_code": "instr",
                        "title": "Spinning Enhanced Visible and InfraRed Imager - SEVIRI-1",
                        "abstract": "The Spinning Enhanced Visible and InfraRed Imager (SEVIRI) instrument measures in 12 spectral channels (compared to only 3 on the previous Meteosat) and records data in a 15 minute cycle (30 minutes on the previous Meteosat). The resolution of the high-resolution visible light channel measures 1 km at the sub-satellite point (compared to 2.5 km on the previous Meteosat).\n\nThe first Meteosat Second Generation satellite, MSG-1, came into operational service on 29th January 2004 and was renamed Meteosat-8. MSG-1 has a nominal lifetime of seven years."
                    },
                    "relatedTo": {
                        "ob_id": 11277,
                        "uuid": "fe1eac4083db49419f3460f3bf828e99",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Spinning Enhanced Visible and InfraRed Imager - SEVIRI-1 at Meteosat Second Generation 1  (MSG-1) or METEOSAT-8 for the Meteosat Second Generation (MSG) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Spinning Enhanced Visible and InfraRed Imager - SEVIRI-1; PLATFORMS: Meteosat Second Generation 1  (MSG-1) or METEOSAT-8; "
                    }
                }
            ]
        },
        {
            "ob_id": 11283,
            "uuid": "f0fe702eb06544c7ac0437a7b4c882b6",
            "short_code": "acq",
            "title": "Acquisition Process for: Met Office Cardington surface meteorological data",
            "abstract": "The Met Office Meteorologial Research Unit located in Cardington, Bedfordshire, operates a wide range of instruments at the surface and on masts at 10, 25 and 50m.",
            "imageDetails": [
                69
            ],
            "mobilePlatformOperation": [],
            "independentInstrument": [
                2410,
                2414,
                2418,
                2422,
                2426,
                2434,
                2442,
                2446,
                2450,
                2454,
                2461,
                4374,
                4378,
                4359,
                4366,
                4386,
                6462,
                6432,
                6458,
                6495,
                2438
            ],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3909,
                    "platform": {
                        "ob_id": 2409,
                        "uuid": "8b8909b3c6fb4b5697fd26cd93e5ac9b",
                        "short_code": "plat",
                        "title": "Met Office Meteorological Research Unit, Cardington",
                        "abstract": "The Meteorological Research Unit, located at Cardington, Bedfordshire (52.10469N. -0.42161 E, 29 m amsl), maintained a suite of surface-based and mast-mounted instrumentation since the 1990s until its closure in 2024. The main purpose of this instrumentation site, which was logged 24 hours a day, was to provide data for atmospheric processes research, and for the development and evaluation of numerical model output and performance.\r\n\r\nThe site has the following identifiers:\r\n- WMO 03559\r\n- DCNN 3456\r\n- WIND 345601\r\n- RAIN 174566\r\n- CLBW 99230\r\n\r\nThe site hosted 3 instrumented towers at 10 m, 25 m and 50 m as well as having capacity to operate radiosonde launches, tethered balloon and UAV flights.\r\n\r\nIn addition, specialist remote-sensing instruments included microwave radiometers, Halo Doppler lidars, and ceilometers.\r\n\r\nFor more specific details for the site see the MIDAS Station entry linked to from this record where the site has a source ID (src_id): 465."
                    },
                    "instrument": {
                        "ob_id": 2430,
                        "uuid": "1f5971a88ad44310bd4b12e5798c8334",
                        "short_code": "instr",
                        "title": "Cardington: Kipp and Zonen CG4 pyrgeometer",
                        "abstract": "Two  Kipp & Zonen   CG4 pyrgeometers are used at the Cardington site, for measuring the incoming and outgoing longwave irradiances (with a spectral range of 4.5 to about 40 mm."
                    },
                    "relatedTo": {
                        "ob_id": 11283,
                        "uuid": "f0fe702eb06544c7ac0437a7b4c882b6",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Met Office Cardington surface meteorological data",
                        "abstract": "The Met Office Meteorologial Research Unit located in Cardington, Bedfordshire, operates a wide range of instruments at the surface and on masts at 10, 25 and 50m."
                    }
                },
                {
                    "ob_id": 4837,
                    "platform": {
                        "ob_id": 11690,
                        "uuid": "b49a0d09007c408bbe425ba8d55e53a2",
                        "short_code": "plat",
                        "title": "50 m tower at the Met Office Meteorological Research Unit, Cardington",
                        "abstract": "The Met Office Meteorological Research Unit, Cardington, use a 50 m tower on which a range of instruments for near-surface observations were deployed."
                    },
                    "instrument": {
                        "ob_id": 2430,
                        "uuid": "1f5971a88ad44310bd4b12e5798c8334",
                        "short_code": "instr",
                        "title": "Cardington: Kipp and Zonen CG4 pyrgeometer",
                        "abstract": "Two  Kipp & Zonen   CG4 pyrgeometers are used at the Cardington site, for measuring the incoming and outgoing longwave irradiances (with a spectral range of 4.5 to about 40 mm."
                    },
                    "relatedTo": {
                        "ob_id": 11283,
                        "uuid": "f0fe702eb06544c7ac0437a7b4c882b6",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Met Office Cardington surface meteorological data",
                        "abstract": "The Met Office Meteorologial Research Unit located in Cardington, Bedfordshire, operates a wide range of instruments at the surface and on masts at 10, 25 and 50m."
                    }
                },
                {
                    "ob_id": 4838,
                    "platform": {
                        "ob_id": 11691,
                        "uuid": "c62617a67e954b129b785e8efd70b16e",
                        "short_code": "plat",
                        "title": "25 m tower at the Met Office Meteorological Research Unit, Cardington",
                        "abstract": "The Met Office Meteorological Research Unit, Cardington, maintain a 25 m tower on which a range of instruments for near-surface observations were deployed."
                    },
                    "instrument": {
                        "ob_id": 2430,
                        "uuid": "1f5971a88ad44310bd4b12e5798c8334",
                        "short_code": "instr",
                        "title": "Cardington: Kipp and Zonen CG4 pyrgeometer",
                        "abstract": "Two  Kipp & Zonen   CG4 pyrgeometers are used at the Cardington site, for measuring the incoming and outgoing longwave irradiances (with a spectral range of 4.5 to about 40 mm."
                    },
                    "relatedTo": {
                        "ob_id": 11283,
                        "uuid": "f0fe702eb06544c7ac0437a7b4c882b6",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Met Office Cardington surface meteorological data",
                        "abstract": "The Met Office Meteorologial Research Unit located in Cardington, Bedfordshire, operates a wide range of instruments at the surface and on masts at 10, 25 and 50m."
                    }
                },
                {
                    "ob_id": 4839,
                    "platform": {
                        "ob_id": 11692,
                        "uuid": "a00869a14a3845a48281c392d865cfec",
                        "short_code": "plat",
                        "title": "10 m tower at the Met Office Meteorological Research Unit, Cardington",
                        "abstract": "The Met Office Meteorological Research Unit, Cardington, maintain a 10 m tower on which a range of instruments for near-surface observations were deployed."
                    },
                    "instrument": {
                        "ob_id": 2430,
                        "uuid": "1f5971a88ad44310bd4b12e5798c8334",
                        "short_code": "instr",
                        "title": "Cardington: Kipp and Zonen CG4 pyrgeometer",
                        "abstract": "Two  Kipp & Zonen   CG4 pyrgeometers are used at the Cardington site, for measuring the incoming and outgoing longwave irradiances (with a spectral range of 4.5 to about 40 mm."
                    },
                    "relatedTo": {
                        "ob_id": 11283,
                        "uuid": "f0fe702eb06544c7ac0437a7b4c882b6",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Met Office Cardington surface meteorological data",
                        "abstract": "The Met Office Meteorologial Research Unit located in Cardington, Bedfordshire, operates a wide range of instruments at the surface and on masts at 10, 25 and 50m."
                    }
                }
            ]
        },
        {
            "ob_id": 11289,
            "uuid": "1024498e8e1e4f2583bdf8a0728e7518",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from FAAM/BAE systems: Liquid and total water content probe (Nevzorov) for the Joint Airborne IASI Validation Experiment (JAIVEX) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: FAAM/BAE systems: Liquid and total water content probe (Nevzorov); ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": []
        },
        {
            "ob_id": 11293,
            "uuid": "9f8340a9d35b4ab38e140893c886c9eb",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from ice-core analysers at North Greenland Ice Coring Project (NGRIP) station for the CRYOspheric STudies of Atmospheric Trends (CRYOSTAT) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ice-core analysers; PLATFORMS: North Greenland Ice Coring Project (NGRIP) station; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3912,
                    "platform": {
                        "ob_id": 1073,
                        "uuid": "0c5d45026ac9485cb1b021c498774de8",
                        "short_code": "plat",
                        "title": "North Greenland Ice Coring Project (NGRIP) station",
                        "abstract": "In the middle of the Greenland ice cap in about 3000 m's height. The NGRIP camp is located at: 75,1 N and 42,3 W."
                    },
                    "instrument": {
                        "ob_id": 11292,
                        "uuid": "a4189c11d52a4da1b404d9e3ef692848",
                        "short_code": "instr",
                        "title": "ice-core analysers",
                        "abstract": "An ice-core analyser is a spectrometer analysing the air trapped in an ice sample."
                    },
                    "relatedTo": {
                        "ob_id": 11293,
                        "uuid": "9f8340a9d35b4ab38e140893c886c9eb",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from ice-core analysers at North Greenland Ice Coring Project (NGRIP) station for the CRYOspheric STudies of Atmospheric Trends (CRYOSTAT) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ice-core analysers; PLATFORMS: North Greenland Ice Coring Project (NGRIP) station; "
                    }
                }
            ]
        },
        {
            "ob_id": 11299,
            "uuid": "4ef9b85ba38c4f099e4bb27189c65c78",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from UEA: Formaldehyde (HCHO) instrument or Fluorometric at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UEA: Formaldehyde (HCHO) instrument or Fluorometric; PLATFORMS: Jungfraujoch, Switzerland; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3913,
                    "platform": {
                        "ob_id": 1523,
                        "uuid": "97bdfb9741f441eebfb16440ebbb0f92",
                        "short_code": "plat",
                        "title": "Jungfraujoch Research Station",
                        "abstract": "The high altitude research station Jungfraujoch (7° 59' E, 46° 32' N, 3580 m a.s.l.) is situated on a mountain saddle in the central Swiss Alps between the Jungfrau (4158 m a.s.l.) in the West and the Moench (4099 m a.s.l.) in the East. The International Foundation High Altitude Research Stations Jungfraujoch and Gornergrat (HFSJG) runs the research station and provides the infrastructure and support for scientific research. Due to its unique place, the year-round accessibility, and the excellent infrastructure, the Jungfraujoch research station is well suited for long-term ground-based monitoring of trace gas concentrations trends in the free troposphere. Due to its location in central Europe and its proximity to anthropogenic greenhouse gas source regions it is also an appropriate study site for European regional source allocations during pollution events. The research activities of EMPA at the Jungfraujoch are conducted within the scope of the Swiss National Air Pollution Monitoring Network (NABEL) funded by the Swiss Federal Office for the Environment (FOEN) and the Global Atmosphere Watch Program (GAW) of the World Meteorological Organization (WMO). The measurement programme at Jungfraujoch includes continuous in-situ analyses of ozone (O3), carbon monoxide (CO), nitrogen monoxide (NO), nitrogen dioxide (NO2), and the sum of nitrogen oxides (NOy). In addition, an extended set of halocarbons and a selection of VOCs (alkanes, aromatics) are measured with a time resolution of four hours since 2000 as a part of SOGE. Daily samples are taken for determination of gaseous SO2 and for particulate sulphur. The concentrations of total suspended particles are continuously observed as well as measured as 48-hour bulk samples. Measurements of methane, nitrous oxide and sulphur hexafluoride were commenced in February 2005 funded by the FOEN. Therefore, the whole set of non-CO2 greenhouse gases is now continuously monitored at the Jungfraujoch."
                    },
                    "instrument": {
                        "ob_id": 196,
                        "uuid": "dac2ad6b673e4e2c9c4973d4f3086251",
                        "short_code": "instr",
                        "title": "UEA: Formaldehyde (HCHO) instrument or Fluorometric",
                        "abstract": "An instrument from the Penkett group at UEA which is flown on research aircrafts to provide 1Hz flourescence measurements of formaldehyde concentration."
                    },
                    "relatedTo": {
                        "ob_id": 11299,
                        "uuid": "4ef9b85ba38c4f099e4bb27189c65c78",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from UEA: Formaldehyde (HCHO) instrument or Fluorometric at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UEA: Formaldehyde (HCHO) instrument or Fluorometric; PLATFORMS: Jungfraujoch, Switzerland; "
                    }
                }
            ]
        },
        {
            "ob_id": 11303,
            "uuid": "c85a3f84cb0146a8a23b931098a5ff5e",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from REMOVE_Leeds: Met Station at Mace Head Research Facility, Ireland for the North Atlantic Marine Boundary Layer EXperiment  (NAMBLEX) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: Mace Head Research Facility, Ireland; PLATFORMS: Mace Head Research Facility, Ireland; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3914,
                    "platform": {
                        "ob_id": 1924,
                        "uuid": "409b3e2004154837805552cb3cb7a546",
                        "short_code": "plat",
                        "title": "Mace Head Atmospheric Research Facility, Ireland",
                        "abstract": "The Mace Head Atmospheric Research Facility is located in Carna, County Galway, Ireland and is managed by the Department of Experimental Physics, Atmospheric Science Group, National University of Ireland, Galway. It has the dual status of a WMO GAW research and monitoring 'global' station and an EMEP supersite. It has the stations ID \"MHD'"
                    },
                    "instrument": {
                        "ob_id": 11302,
                        "uuid": "d7796b0819d64529a62a94e300d389e4",
                        "short_code": "instr",
                        "title": "UNDEFINED instrument associated with platform: Mace Head Research Facility, Ireland",
                        "abstract": "This instrument is associated with the platform: Mace Head Research Facility, Ireland"
                    },
                    "relatedTo": {
                        "ob_id": 11303,
                        "uuid": "c85a3f84cb0146a8a23b931098a5ff5e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from REMOVE_Leeds: Met Station at Mace Head Research Facility, Ireland for the North Atlantic Marine Boundary Layer EXperiment  (NAMBLEX) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: Mace Head Research Facility, Ireland; PLATFORMS: Mace Head Research Facility, Ireland; "
                    }
                }
            ]
        },
        {
            "ob_id": 11306,
            "uuid": "19cac875128e4113bb106abf61cfdf8c",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Met Office C-band radar at Chenies Radar Station, UK",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office C-band radar; PLATFORMS: Chenies Radar Station, UK; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3915,
                    "platform": {
                        "ob_id": 998,
                        "uuid": "2360f9cfe5f246b0b83877fb9d51497f",
                        "short_code": "plat",
                        "title": "Chenies Radar Station, UK",
                        "abstract": "Station in the UK rain radar network, located at Flauden near Amersham, UK."
                    },
                    "instrument": {
                        "ob_id": 1003,
                        "uuid": "fe89d9092055426eb719290ce4063b88",
                        "short_code": "instr",
                        "title": "Met Office C-band radar",
                        "abstract": "UK C Band radar run by the Met Office and the Environment Agency."
                    },
                    "relatedTo": {
                        "ob_id": 11306,
                        "uuid": "19cac875128e4113bb106abf61cfdf8c",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Met Office C-band radar at Chenies Radar Station, UK",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office C-band radar; PLATFORMS: Chenies Radar Station, UK; "
                    }
                }
            ]
        },
        {
            "ob_id": 11309,
            "uuid": "7c64a455cb2643d986c3c92f5656256f",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from EMPA: GC-ECD at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: EMPA: GC-ECD; PLATFORMS: Jungfraujoch, Switzerland; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3916,
                    "platform": {
                        "ob_id": 1523,
                        "uuid": "97bdfb9741f441eebfb16440ebbb0f92",
                        "short_code": "plat",
                        "title": "Jungfraujoch Research Station",
                        "abstract": "The high altitude research station Jungfraujoch (7° 59' E, 46° 32' N, 3580 m a.s.l.) is situated on a mountain saddle in the central Swiss Alps between the Jungfrau (4158 m a.s.l.) in the West and the Moench (4099 m a.s.l.) in the East. The International Foundation High Altitude Research Stations Jungfraujoch and Gornergrat (HFSJG) runs the research station and provides the infrastructure and support for scientific research. Due to its unique place, the year-round accessibility, and the excellent infrastructure, the Jungfraujoch research station is well suited for long-term ground-based monitoring of trace gas concentrations trends in the free troposphere. Due to its location in central Europe and its proximity to anthropogenic greenhouse gas source regions it is also an appropriate study site for European regional source allocations during pollution events. The research activities of EMPA at the Jungfraujoch are conducted within the scope of the Swiss National Air Pollution Monitoring Network (NABEL) funded by the Swiss Federal Office for the Environment (FOEN) and the Global Atmosphere Watch Program (GAW) of the World Meteorological Organization (WMO). The measurement programme at Jungfraujoch includes continuous in-situ analyses of ozone (O3), carbon monoxide (CO), nitrogen monoxide (NO), nitrogen dioxide (NO2), and the sum of nitrogen oxides (NOy). In addition, an extended set of halocarbons and a selection of VOCs (alkanes, aromatics) are measured with a time resolution of four hours since 2000 as a part of SOGE. Daily samples are taken for determination of gaseous SO2 and for particulate sulphur. The concentrations of total suspended particles are continuously observed as well as measured as 48-hour bulk samples. Measurements of methane, nitrous oxide and sulphur hexafluoride were commenced in February 2005 funded by the FOEN. Therefore, the whole set of non-CO2 greenhouse gases is now continuously monitored at the Jungfraujoch."
                    },
                    "instrument": {
                        "ob_id": 2923,
                        "uuid": "2f67f2b572884de0ac8bce1e54710ba8",
                        "short_code": "instr",
                        "title": "EMPA: GC-ECD",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11309,
                        "uuid": "7c64a455cb2643d986c3c92f5656256f",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from EMPA: GC-ECD at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: EMPA: GC-ECD; PLATFORMS: Jungfraujoch, Switzerland; "
                    }
                }
            ]
        },
        {
            "ob_id": 11312,
            "uuid": "99b8bcf64b9d4be0a762f7ebe98ea8f9",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Leicester: Spectral Radiometer j(NO2) at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Leicester: Spectral Radiometer j(NO2); PLATFORMS: Jungfraujoch, Switzerland; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3917,
                    "platform": {
                        "ob_id": 1523,
                        "uuid": "97bdfb9741f441eebfb16440ebbb0f92",
                        "short_code": "plat",
                        "title": "Jungfraujoch Research Station",
                        "abstract": "The high altitude research station Jungfraujoch (7° 59' E, 46° 32' N, 3580 m a.s.l.) is situated on a mountain saddle in the central Swiss Alps between the Jungfrau (4158 m a.s.l.) in the West and the Moench (4099 m a.s.l.) in the East. The International Foundation High Altitude Research Stations Jungfraujoch and Gornergrat (HFSJG) runs the research station and provides the infrastructure and support for scientific research. Due to its unique place, the year-round accessibility, and the excellent infrastructure, the Jungfraujoch research station is well suited for long-term ground-based monitoring of trace gas concentrations trends in the free troposphere. Due to its location in central Europe and its proximity to anthropogenic greenhouse gas source regions it is also an appropriate study site for European regional source allocations during pollution events. The research activities of EMPA at the Jungfraujoch are conducted within the scope of the Swiss National Air Pollution Monitoring Network (NABEL) funded by the Swiss Federal Office for the Environment (FOEN) and the Global Atmosphere Watch Program (GAW) of the World Meteorological Organization (WMO). The measurement programme at Jungfraujoch includes continuous in-situ analyses of ozone (O3), carbon monoxide (CO), nitrogen monoxide (NO), nitrogen dioxide (NO2), and the sum of nitrogen oxides (NOy). In addition, an extended set of halocarbons and a selection of VOCs (alkanes, aromatics) are measured with a time resolution of four hours since 2000 as a part of SOGE. Daily samples are taken for determination of gaseous SO2 and for particulate sulphur. The concentrations of total suspended particles are continuously observed as well as measured as 48-hour bulk samples. Measurements of methane, nitrous oxide and sulphur hexafluoride were commenced in February 2005 funded by the FOEN. Therefore, the whole set of non-CO2 greenhouse gases is now continuously monitored at the Jungfraujoch."
                    },
                    "instrument": {
                        "ob_id": 311,
                        "uuid": "fe82ff833eaf4a9593134c237b303dc2",
                        "short_code": "instr",
                        "title": "Leicester: Spectral Radiometer j(NO2)",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11312,
                        "uuid": "99b8bcf64b9d4be0a762f7ebe98ea8f9",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Leicester: Spectral Radiometer j(NO2) at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Leicester: Spectral Radiometer j(NO2); PLATFORMS: Jungfraujoch, Switzerland; "
                    }
                }
            ]
        },
        {
            "ob_id": 11315,
            "uuid": "aece11c868804c6789483724c01948de",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Automatic Weather Station (AWS) at Global Weather Stations for the Met Office",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Automatic Weather Station (AWS); PLATFORMS: Global Weather Stations; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
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                    "platform": {
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                        "uuid": "3b6733ebdc034bd58c8d1f9e853dbdd1",
                        "short_code": "plat",
                        "title": "Global Weather Stations",
                        "abstract": "global weather stations as used by MIDAS."
                    },
                    "instrument": {
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                        "uuid": "a2f40afd5f054601a037d48a9aac17e9",
                        "short_code": "instr",
                        "title": "Automatic Weather Station (AWS)",
                        "abstract": "An automatic weather station (AWS) is an automated version of the traditional weather station, either to save human labour or to enable measurements from remote areas. The system may report in near real time via ARGOS and the Global telecommunications system, or save the data for later recovery."
                    },
                    "relatedTo": {
                        "ob_id": 11315,
                        "uuid": "aece11c868804c6789483724c01948de",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Automatic Weather Station (AWS) at Global Weather Stations for the Met Office",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Automatic Weather Station (AWS); PLATFORMS: Global Weather Stations; "
                    }
                }
            ]
        },
        {
            "ob_id": 11319,
            "uuid": "ae018fb2fdac47f8aeaf9db7f6b71152",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from NIMBUS 5 Selective Chopper Radiometer (SCR) at NIMBUS 5 satellite for the NASA - National Aeronautics and Space Administration",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: NIMBUS 5 Selective Chopper Radiometer (SCR); PLATFORMS: NIMBUS 5 satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 5514,
                    "uuid": "c19617640bcc48df98d97f5c6f9810f9",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: NIMBUS 5 satellite",
                    "abstract": "Mobile Platform Operation related to the: NIMBUS 5 satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3919,
                    "platform": {
                        "ob_id": 5512,
                        "uuid": "bd14245375844b1ba0869f1f672f09fc",
                        "short_code": "plat",
                        "title": "NIMBUS 5 satellite",
                        "abstract": "NASA polar-orbiting spacecraft designed to serve as a stabilized, earth-oriented platform for the testing of advanced meteorological sensor systems and collecting meteorological and geological data on a global scale. It was launched on 11th December 1972."
                    },
                    "instrument": {
                        "ob_id": 5513,
                        "uuid": "0c010dfea4344e58bff912e55e442df0",
                        "short_code": "instr",
                        "title": "NIMBUS 5 Selective Chopper Radiometer (SCR)",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11319,
                        "uuid": "ae018fb2fdac47f8aeaf9db7f6b71152",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from NIMBUS 5 Selective Chopper Radiometer (SCR) at NIMBUS 5 satellite for the NASA - National Aeronautics and Space Administration",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: NIMBUS 5 Selective Chopper Radiometer (SCR); PLATFORMS: NIMBUS 5 satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 11326,
            "uuid": "a82e936d265b426c8d4202af7e085c11",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Leicester: Spectral Radiometer j(O1D) at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Leicester: Spectral Radiometer j(O1D); PLATFORMS: Jungfraujoch, Switzerland; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3920,
                    "platform": {
                        "ob_id": 1523,
                        "uuid": "97bdfb9741f441eebfb16440ebbb0f92",
                        "short_code": "plat",
                        "title": "Jungfraujoch Research Station",
                        "abstract": "The high altitude research station Jungfraujoch (7° 59' E, 46° 32' N, 3580 m a.s.l.) is situated on a mountain saddle in the central Swiss Alps between the Jungfrau (4158 m a.s.l.) in the West and the Moench (4099 m a.s.l.) in the East. The International Foundation High Altitude Research Stations Jungfraujoch and Gornergrat (HFSJG) runs the research station and provides the infrastructure and support for scientific research. Due to its unique place, the year-round accessibility, and the excellent infrastructure, the Jungfraujoch research station is well suited for long-term ground-based monitoring of trace gas concentrations trends in the free troposphere. Due to its location in central Europe and its proximity to anthropogenic greenhouse gas source regions it is also an appropriate study site for European regional source allocations during pollution events. The research activities of EMPA at the Jungfraujoch are conducted within the scope of the Swiss National Air Pollution Monitoring Network (NABEL) funded by the Swiss Federal Office for the Environment (FOEN) and the Global Atmosphere Watch Program (GAW) of the World Meteorological Organization (WMO). The measurement programme at Jungfraujoch includes continuous in-situ analyses of ozone (O3), carbon monoxide (CO), nitrogen monoxide (NO), nitrogen dioxide (NO2), and the sum of nitrogen oxides (NOy). In addition, an extended set of halocarbons and a selection of VOCs (alkanes, aromatics) are measured with a time resolution of four hours since 2000 as a part of SOGE. Daily samples are taken for determination of gaseous SO2 and for particulate sulphur. The concentrations of total suspended particles are continuously observed as well as measured as 48-hour bulk samples. Measurements of methane, nitrous oxide and sulphur hexafluoride were commenced in February 2005 funded by the FOEN. Therefore, the whole set of non-CO2 greenhouse gases is now continuously monitored at the Jungfraujoch."
                    },
                    "instrument": {
                        "ob_id": 315,
                        "uuid": "6e6a11c756bf49e48dca59ca002f351b",
                        "short_code": "instr",
                        "title": "Leicester: Spectral Radiometer j(O1D)",
                        "abstract": "Instrument.abstract: DETAILS NEEDED"
                    },
                    "relatedTo": {
                        "ob_id": 11326,
                        "uuid": "a82e936d265b426c8d4202af7e085c11",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Leicester: Spectral Radiometer j(O1D) at Jungfraujoch, Switzerland for the ACSOE (Atmosphere Chemistry Studies in the Oceanic Environment) - OXIdising Capacity of the Ocean Atmosphere (OXICOA) Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Leicester: Spectral Radiometer j(O1D); PLATFORMS: Jungfraujoch, Switzerland; "
                    }
                }
            ]
        },
        {
            "ob_id": 11329,
            "uuid": "cbd6eba17fdc441797beba8ede98e779",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Reading University Observatory: 3-cup anemometer and wind vane at Reading University Atmospheric Observatory for the UTLS-OZONE NERC Research Programme Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Reading University Observatory: 3-cup anemometer and wind vane; PLATFORMS: Reading University Atmospheric Observatory; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3921,
                    "platform": {
                        "ob_id": 1878,
                        "uuid": "dad6ee58123d405cb3d7afa5f3d29d7d",
                        "short_code": "plat",
                        "title": "University of Reading Atmospheric Observatory",
                        "abstract": "The University of Reading Atmospheric Observatory has been a centre for atmospheric measurements and meteorological observations since 1970, continuing records which began originally at the University College of Reading in 1900. The observatory is situated on the Whiteknights campus (51.442 deg N, 0.938 deg W), near the Earley Gate entrance, at 66m above sea level.\r\nIt is an urban site, located within the town of Reading (population 150, 000).  The site is on a flat piece of land, covered by grass all year round.  As well as traditional meteorological observation and automatic continuous meteorological measurements the site is also used for potential gradient (PG) measurements, leading to a large number of metal posts nearby, including a 10m tower and two 10m poles.\r\n "
                    },
                    "instrument": {
                        "ob_id": 1883,
                        "uuid": "096e221a59a04d269df80d4dc0363681",
                        "short_code": "instr",
                        "title": "Reading University Observatory: 3-cup anemometer and wind vane",
                        "abstract": "Wind measurements are made on the southern of the field site at 3m above the surface using a wind vane and a three-cup anemometer.Both devices were manufactured by Vector Instruments."
                    },
                    "relatedTo": {
                        "ob_id": 11329,
                        "uuid": "cbd6eba17fdc441797beba8ede98e779",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Reading University Observatory: 3-cup anemometer and wind vane at Reading University Atmospheric Observatory for the UTLS-OZONE NERC Research Programme Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Reading University Observatory: 3-cup anemometer and wind vane; PLATFORMS: Reading University Atmospheric Observatory; "
                    }
                }
            ]
        },
        {
            "ob_id": 11335,
            "uuid": "79b51370db19447cac4b36f87245ba52",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Met Office station observer - NCM message at Met Office Synoptic network for the Met Office",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office station observer - NCM message; PLATFORMS: Met Office Synoptic network; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 3922,
                    "platform": {
                        "ob_id": 4358,
                        "uuid": "9831a159981241f8be4b7dae150342c8",
                        "short_code": "plat",
                        "title": "Met Office Synoptic network",
                        "abstract": "The synoptic network meets the requirements of forecasting, nowcasting, NWP and international exchange for real time observations taken at intervals between 1 and 3 hours. The observed elements include weather, cloud, temperature, humidity, wind, visibility, pressure etc. contained in the SYNOP message."
                    },
                    "instrument": {
                        "ob_id": 6495,
                        "uuid": "6d29c988efc34f3eab98881f183c4c07",
                        "short_code": "instr",
                        "title": "Met Office station observer - NCM message",
                        "abstract": "Observer reporting daily and hourly specific weather parameters which cannot be measured by an instrument e.g. cloud type, cloud amount, present and past weather and state of ground."
                    },
                    "relatedTo": {
                        "ob_id": 11335,
                        "uuid": "79b51370db19447cac4b36f87245ba52",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Met Office station observer - NCM message at Met Office Synoptic network for the Met Office",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Met Office station observer - NCM message; PLATFORMS: Met Office Synoptic network; "
                    }
                }
            ]
        }
    ]
}