Procedure Acquisition List

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{
    "count": 5833,
    "next": "https://api.catalogue.ceda.ac.uk/api/v3/acquisitions/?format=api&limit=100&offset=1900",
    "previous": "https://api.catalogue.ceda.ac.uk/api/v3/acquisitions/?format=api&limit=100&offset=1700",
    "results": [
        {
            "ob_id": 8210,
            "uuid": "eec8d2e5b2f14fd7b69e8f209b23ac4a",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from GOME-2 at Metop-A for the Eumetsat Polar System Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: GOME-2; 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": 2564,
                    "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": 8208,
                        "uuid": "b2dd8e99b1944c5ca964b6baa8e0877f",
                        "short_code": "instr",
                        "title": "GOME-2",
                        "abstract": "Data from the GOME-2 instrument on board the Eumetsat EPS MetOp satellite. GOME-2 is a spectrometer that measures both the radiance component of the light reflected by the Sun-illuminated Earth's atmosphere and the direct Sun light. The measurements are used to obtain detailed information on global trace gas distributions of ozone, nitrogen dioxide, water vapor, bromine oxide and other trace gases as well as aerosol properties."
                    },
                    "relatedTo": {
                        "ob_id": 8210,
                        "uuid": "eec8d2e5b2f14fd7b69e8f209b23ac4a",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from GOME-2 at Metop-A for the Eumetsat Polar System Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: GOME-2; PLATFORMS: Metop-A; "
                    }
                }
            ]
        },
        {
            "ob_id": 8218,
            "uuid": "e983134657a94a2ba74dfcf5705f0b20",
            "short_code": "acq",
            "title": "Acquisition Process for: Advanced Visible and Near InfraRed Radiometer type 2 (AVNIR 2) UK data",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Advanced Visible and Near InfraRed Radiometer type 2 (AVNIR 2); PLATFORMS: Advanced Land Observing Satellite (ALOS); ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8199,
                    "uuid": "93636a8dcd044aa7a9edf04efb2c1b40",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Advanced Land Observing Satellite (ALOS)",
                    "abstract": "Mobile Platform Operation related to the: Advanced Land Observing Satellite (ALOS)"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2565,
                    "platform": {
                        "ob_id": 8197,
                        "uuid": "68af680aef294055a33e69ebb83a3e6e",
                        "short_code": "plat",
                        "title": "Advanced Land Observing Satellite (ALOS)",
                        "abstract": "The Advanced Land Observing Satellite (ALOS) hosts the Advanced Visible and Near-Infrared Radiometer type 2 (AVNIR-2), the Panchromatic Remote sensing Instrument for Stereo Mapping (PRISM) and the Phased Array type-L band Synthetic Aperture Radar (PALSAR). The satellite, developed by the Japan Aerospace Exploration Agency (JAXA), was launched in 2006 and was active for 5 years. It has since lost power, but remains in orbit. It's mission included cartography, regional observation, disaster monitoring and resource surveying."
                    },
                    "instrument": {
                        "ob_id": 8216,
                        "uuid": "114f2dcda40c42c68a51d6abaddf31d5",
                        "short_code": "instr",
                        "title": "Advanced Visible and Near InfraRed Radiometer type 2 (AVNIR 2)",
                        "abstract": "The Advanced Visible and Near InfraRed 4-band Radiometer type-2 (AVNIR-2) is a visible and near infrared 4-band radiometer offering 10m spatial resolution optical imagery that is often used for land and coastal earth observation applications. AVNIR-2 is on board the Japanese earth observation Advanced Land Observing Satellite (ALOS) and was developed by the Japanese Aerospace Exploration Agency (JAXA). The satellite was launched in 2006 and was active for 5 years. It has since lost power, but remains in orbit as of July 2014. Data are available for large areas of the Republic of Ireland and small areas of Scotland and England, for 2007 to 2008."
                    },
                    "relatedTo": {
                        "ob_id": 8218,
                        "uuid": "e983134657a94a2ba74dfcf5705f0b20",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Advanced Visible and Near InfraRed Radiometer type 2 (AVNIR 2) UK data",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Advanced Visible and Near InfraRed Radiometer type 2 (AVNIR 2); PLATFORMS: Advanced Land Observing Satellite (ALOS); "
                    }
                }
            ]
        },
        {
            "ob_id": 8224,
            "uuid": "9c33997b2ca440a081030bd4fdec6de6",
            "short_code": "acq",
            "title": "Acquisition Process for: Colour InfraRed (CIR) data for England and Wales",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Vexel UltraCam, ADS40 from Leica Geosystems; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [
                8222,
                8223
            ],
            "instrumentplatformpair_set": []
        },
        {
            "ob_id": 8235,
            "uuid": "882dd21b0c2643f68eb10f2b10790532",
            "short_code": "acq",
            "title": "Acquisition Process for: Disaster Monitoring Constellation (DMC) UK imagery",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Surrey Linear Imager Multispectral 6 channels (SLIM-6) sensor, Surrey Linear Imager Multispectral 6 channels - 22-metre (SLIM-6-22) sensor; PLATFORMS: UK Disaster Monitoring Constellation (UK-DMC) satellite, UK Disaster Monitoring Constellation 2 (UK-DMC2) satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8233,
                    "uuid": "fcbdea3c564e434191d11034ea6f1781",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: UK Disaster Monitoring Constellation (UK-DMC) satellite",
                    "abstract": "Mobile Platform Operation related to the: UK Disaster Monitoring Constellation (UK-DMC) satellite"
                },
                {
                    "ob_id": 8234,
                    "uuid": "b4c20c44f6c04ad29a7a0a8c1ceeefae",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: UK Disaster Monitoring Constellation 2 (UK-DMC2) satellite",
                    "abstract": "Mobile Platform Operation related to the: UK Disaster Monitoring Constellation 2 (UK-DMC2) satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2566,
                    "platform": {
                        "ob_id": 8229,
                        "uuid": "8b20ed9d163a4ce9ac7055a6cf92e6a3",
                        "short_code": "plat",
                        "title": "UK Disaster Monitoring Constellation (UK-DMC) satellite",
                        "abstract": "The first generation UK Disaster Monitoring Constellation (UK-DMC) satellite was launched in 2002-3 by Surrey Satellite Technology Ltd to create the first constellation designed to deliver daily repeat high resolution imaging."
                    },
                    "instrument": {
                        "ob_id": 8231,
                        "uuid": "c8b791ccdc184285baa49a431c13c674",
                        "short_code": "instr",
                        "title": "Surrey Linear Imager Multispectral 6 channels (SLIM-6) sensor",
                        "abstract": "The SLIM-6 imager is a dual bank linear Charge Coupled Device (CCD) push broom imager utilising the orbital motion of the Disaster Monitoring Constellation (DMC) platform to capture radiation reflected from the Earth’s surface within a 600km swath at a spatial resolution of approximately 32m."
                    },
                    "relatedTo": {
                        "ob_id": 8235,
                        "uuid": "882dd21b0c2643f68eb10f2b10790532",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Disaster Monitoring Constellation (DMC) UK imagery",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Surrey Linear Imager Multispectral 6 channels (SLIM-6) sensor, Surrey Linear Imager Multispectral 6 channels - 22-metre (SLIM-6-22) sensor; PLATFORMS: UK Disaster Monitoring Constellation (UK-DMC) satellite, UK Disaster Monitoring Constellation 2 (UK-DMC2) satellite; "
                    }
                },
                {
                    "ob_id": 2567,
                    "platform": {
                        "ob_id": 8229,
                        "uuid": "8b20ed9d163a4ce9ac7055a6cf92e6a3",
                        "short_code": "plat",
                        "title": "UK Disaster Monitoring Constellation (UK-DMC) satellite",
                        "abstract": "The first generation UK Disaster Monitoring Constellation (UK-DMC) satellite was launched in 2002-3 by Surrey Satellite Technology Ltd to create the first constellation designed to deliver daily repeat high resolution imaging."
                    },
                    "instrument": {
                        "ob_id": 8232,
                        "uuid": "4afc4f50640a47c1a2e712c4364b8bb7",
                        "short_code": "instr",
                        "title": "Surrey Linear Imager Multispectral 6 channels - 22-metre (SLIM-6-22) sensor",
                        "abstract": "The SLIM-6 imager is a dual bank linear Charge Coupled Device (CCD) push broom imager utilising the orbital motion of the Disaster Monitoring Constellation (DMC) platform to capture radiation reflected from the Earth’s surface within a 600km swath at a spatial resolution of approximately 22m."
                    },
                    "relatedTo": {
                        "ob_id": 8235,
                        "uuid": "882dd21b0c2643f68eb10f2b10790532",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Disaster Monitoring Constellation (DMC) UK imagery",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Surrey Linear Imager Multispectral 6 channels (SLIM-6) sensor, Surrey Linear Imager Multispectral 6 channels - 22-metre (SLIM-6-22) sensor; PLATFORMS: UK Disaster Monitoring Constellation (UK-DMC) satellite, UK Disaster Monitoring Constellation 2 (UK-DMC2) satellite; "
                    }
                },
                {
                    "ob_id": 2568,
                    "platform": {
                        "ob_id": 8230,
                        "uuid": "93faef63da3c470c907d387eade3f513",
                        "short_code": "plat",
                        "title": "UK Disaster Monitoring Constellation 2 (UK-DMC2) satellite",
                        "abstract": "The second generation DMC satellite, launched 2009, provides hugely increased imaging capacity over the original UK-DMC satellite, retaining the same 650km swath width, but with twice the pixel density at 22m Ground Sample Distance (GSD)."
                    },
                    "instrument": {
                        "ob_id": 8231,
                        "uuid": "c8b791ccdc184285baa49a431c13c674",
                        "short_code": "instr",
                        "title": "Surrey Linear Imager Multispectral 6 channels (SLIM-6) sensor",
                        "abstract": "The SLIM-6 imager is a dual bank linear Charge Coupled Device (CCD) push broom imager utilising the orbital motion of the Disaster Monitoring Constellation (DMC) platform to capture radiation reflected from the Earth’s surface within a 600km swath at a spatial resolution of approximately 32m."
                    },
                    "relatedTo": {
                        "ob_id": 8235,
                        "uuid": "882dd21b0c2643f68eb10f2b10790532",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Disaster Monitoring Constellation (DMC) UK imagery",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Surrey Linear Imager Multispectral 6 channels (SLIM-6) sensor, Surrey Linear Imager Multispectral 6 channels - 22-metre (SLIM-6-22) sensor; PLATFORMS: UK Disaster Monitoring Constellation (UK-DMC) satellite, UK Disaster Monitoring Constellation 2 (UK-DMC2) satellite; "
                    }
                },
                {
                    "ob_id": 2569,
                    "platform": {
                        "ob_id": 8230,
                        "uuid": "93faef63da3c470c907d387eade3f513",
                        "short_code": "plat",
                        "title": "UK Disaster Monitoring Constellation 2 (UK-DMC2) satellite",
                        "abstract": "The second generation DMC satellite, launched 2009, provides hugely increased imaging capacity over the original UK-DMC satellite, retaining the same 650km swath width, but with twice the pixel density at 22m Ground Sample Distance (GSD)."
                    },
                    "instrument": {
                        "ob_id": 8232,
                        "uuid": "4afc4f50640a47c1a2e712c4364b8bb7",
                        "short_code": "instr",
                        "title": "Surrey Linear Imager Multispectral 6 channels - 22-metre (SLIM-6-22) sensor",
                        "abstract": "The SLIM-6 imager is a dual bank linear Charge Coupled Device (CCD) push broom imager utilising the orbital motion of the Disaster Monitoring Constellation (DMC) platform to capture radiation reflected from the Earth’s surface within a 600km swath at a spatial resolution of approximately 22m."
                    },
                    "relatedTo": {
                        "ob_id": 8235,
                        "uuid": "882dd21b0c2643f68eb10f2b10790532",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Disaster Monitoring Constellation (DMC) UK imagery",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Surrey Linear Imager Multispectral 6 channels (SLIM-6) sensor, Surrey Linear Imager Multispectral 6 channels - 22-metre (SLIM-6-22) sensor; PLATFORMS: UK Disaster Monitoring Constellation (UK-DMC) satellite, UK Disaster Monitoring Constellation 2 (UK-DMC2) satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 8251,
            "uuid": "1549d4e36c8040da933103f7bbeaf215",
            "short_code": "acq",
            "title": "Acquisition Process for: UK Landsat 4/5 imagery acquired by Landmap from Infoterra",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Landsat MSS (MultiSpectral Scanner), Landsat Thematic Mapper (TM); PLATFORMS: Landsat 4, Landsat 5; ",
            "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"
                },
                {
                    "ob_id": 8250,
                    "uuid": "4894a74f37cb49ea99a6b7d7669228e4",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Landsat 5",
                    "abstract": "Mobile Platform Operation related to the: Landsat 5"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2570,
                    "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": 8247,
                        "uuid": "9bf3c7a69d84430280bd72c0e63a119c",
                        "short_code": "instr",
                        "title": "Landsat MSS (MultiSpectral Scanner)",
                        "abstract": "The Multispectral Scanner is one of the Earth observing sensors introduced in the Landsat program. A Multispectral Scanner (MSS) was placed aboard each of the first five Landsat satellites. The MSS' on Landsat 4 and 5 were capable of detecting radiation in 5 bands between 0.5 and 1.1µm as opposed to 4 on Landsat 1, 2 and 3."
                    },
                    "relatedTo": {
                        "ob_id": 8251,
                        "uuid": "1549d4e36c8040da933103f7bbeaf215",
                        "short_code": "acq",
                        "title": "Acquisition Process for: UK Landsat 4/5 imagery acquired by Landmap from Infoterra",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Landsat MSS (MultiSpectral Scanner), Landsat Thematic Mapper (TM); PLATFORMS: Landsat 4, Landsat 5; "
                    }
                },
                {
                    "ob_id": 2571,
                    "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": 8248,
                        "uuid": "c7d350b1ec99448187607ec46c4ce35e",
                        "short_code": "instr",
                        "title": "Landsat Thematic Mapper (TM)",
                        "abstract": "The Thematic Mapper (TM) is one of the Earth observing sensors introduced in the Landsat program. TMs were placed aboard the Landsat 4 and 5 satellites. The wavelength range for the Thematic Mapper (TM) sensor is from the visible, through the Mid-IR, into the Thermal-IR portion of the electromagnetic spectrum."
                    },
                    "relatedTo": {
                        "ob_id": 8251,
                        "uuid": "1549d4e36c8040da933103f7bbeaf215",
                        "short_code": "acq",
                        "title": "Acquisition Process for: UK Landsat 4/5 imagery acquired by Landmap from Infoterra",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Landsat MSS (MultiSpectral Scanner), Landsat Thematic Mapper (TM); PLATFORMS: Landsat 4, Landsat 5; "
                    }
                },
                {
                    "ob_id": 2572,
                    "platform": {
                        "ob_id": 8246,
                        "uuid": "e9c4a76ba5b64ede82a20d7d69da47a2",
                        "short_code": "plat",
                        "title": "Landsat 5",
                        "abstract": "A nearly identical satellite to Landsat 4, Landsat 5 was launched as part of the Landsat programme in March 1984 and was operational until June 2013. As Landsat 4, it carried Thematic Mapper (TM) and MultiSpectral Scanner (MSS) instruments."
                    },
                    "instrument": {
                        "ob_id": 8247,
                        "uuid": "9bf3c7a69d84430280bd72c0e63a119c",
                        "short_code": "instr",
                        "title": "Landsat MSS (MultiSpectral Scanner)",
                        "abstract": "The Multispectral Scanner is one of the Earth observing sensors introduced in the Landsat program. A Multispectral Scanner (MSS) was placed aboard each of the first five Landsat satellites. The MSS' on Landsat 4 and 5 were capable of detecting radiation in 5 bands between 0.5 and 1.1µm as opposed to 4 on Landsat 1, 2 and 3."
                    },
                    "relatedTo": {
                        "ob_id": 8251,
                        "uuid": "1549d4e36c8040da933103f7bbeaf215",
                        "short_code": "acq",
                        "title": "Acquisition Process for: UK Landsat 4/5 imagery acquired by Landmap from Infoterra",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Landsat MSS (MultiSpectral Scanner), Landsat Thematic Mapper (TM); PLATFORMS: Landsat 4, Landsat 5; "
                    }
                },
                {
                    "ob_id": 2573,
                    "platform": {
                        "ob_id": 8246,
                        "uuid": "e9c4a76ba5b64ede82a20d7d69da47a2",
                        "short_code": "plat",
                        "title": "Landsat 5",
                        "abstract": "A nearly identical satellite to Landsat 4, Landsat 5 was launched as part of the Landsat programme in March 1984 and was operational until June 2013. As Landsat 4, it carried Thematic Mapper (TM) and MultiSpectral Scanner (MSS) instruments."
                    },
                    "instrument": {
                        "ob_id": 8248,
                        "uuid": "c7d350b1ec99448187607ec46c4ce35e",
                        "short_code": "instr",
                        "title": "Landsat Thematic Mapper (TM)",
                        "abstract": "The Thematic Mapper (TM) is one of the Earth observing sensors introduced in the Landsat program. TMs were placed aboard the Landsat 4 and 5 satellites. The wavelength range for the Thematic Mapper (TM) sensor is from the visible, through the Mid-IR, into the Thermal-IR portion of the electromagnetic spectrum."
                    },
                    "relatedTo": {
                        "ob_id": 8251,
                        "uuid": "1549d4e36c8040da933103f7bbeaf215",
                        "short_code": "acq",
                        "title": "Acquisition Process for: UK Landsat 4/5 imagery acquired by Landmap from Infoterra",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Landsat MSS (MultiSpectral Scanner), Landsat Thematic Mapper (TM); PLATFORMS: Landsat 4, Landsat 5; "
                    }
                }
            ]
        },
        {
            "ob_id": 8259,
            "uuid": "535c053640594563ba18f8773f812e86",
            "short_code": "acq",
            "title": "Acquisition Process for: Landsat 7 data acquired by Landmap from Infoterra",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Enhanced Thematic Mapper Plus (ETM+); PLATFORMS: Landsat 7; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8258,
                    "uuid": "09bcf80950014799ad6e2bdb9ce4a74e",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Landsat 7",
                    "abstract": "Mobile Platform Operation related to the: Landsat 7"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2574,
                    "platform": {
                        "ob_id": 8256,
                        "uuid": "385d8284709749b9a29d33c07670c4fd",
                        "short_code": "plat",
                        "title": "Landsat 7",
                        "abstract": "Landsat 7 was launched as a continuation of the Landsat programme on 15th April 1999 and is still operational as of July 2014. A three-axis attitude control subsystem stabilizes the satellite and keeps the instrument pointed toward Earth to within 0.05 degrees. The LANDSAT World-Wide-Reference system catalogues the worlds land mass into 57,784 scenes, each 115 miles (183 kilometres) wide by 106 miles (170 kilometres) long.\r\n\r\nLaunch date:  15/04/1999\r\nStatus/projected mission lifetime:  5 years +\r\nOrbit parameters:  near circular\r\nNominal altitude:  705 km\r\nOrbit type:\t near-polar, sun-synchronous\r\nInclination:  98.2 degrees\r\nRepeat period:  16 days\r\nEquatorial crossing time:  10.00 local time (descending node)\r\nSwath width:  183 km\r\nResolution:  15 - 60 m \r\nSpecial features:  Panchromatic band, thermal band with 2 gain settings"
                    },
                    "instrument": {
                        "ob_id": 8257,
                        "uuid": "dfc450e6a1d54b40b8927c7d0de2de21",
                        "short_code": "instr",
                        "title": "Enhanced Thematic Mapper Plus (ETM+)",
                        "abstract": "The Enhanced Thematic Mapper Plus (ETM+) instrument is a fixed 'whisk-broom', eight-band, multispectral scanning radiometer capable of providing high-resolution imaging information of the Earth's surface onboard Landsat 7. The main improvement from the Landsat 4/5 Thematic Mappers (TMs) is the addition of a panchromatic band with 15 m spatial resolution.\r\nSpectral and spatial characteristics of these bands are shown below.\r\n\r\nBand no. 1\r\nSpectral range .450 to .515 micrometres Ground resolution: 30 m\r\nBand no. 2\r\nSpectral range .525 to .605 micrometres Ground resolution: 30 m\r\nBand no. 3\r\nSpectral range .630 to .690 micrometres Ground resolution: 30 m\r\nBand no. 4\r\nSpectral range .775 to .900 micrometres Ground resolution: 30 m\r\nBand no. 5\r\nSpectral range 1.550 to 1.750 micrometres Ground resolution: 30 m\r\nBand no. 6\r\nSpectral range 10.40 to 12.50 micrometres Ground resolution: 60 m\r\nBand no. 7\r\nSpectral range 2.090 to 2.35 micrometres Ground resolution: 30 m\r\nBand no. 8\r\nSpectral range .520 to .900 micrometres Ground resolution: 15 m"
                    },
                    "relatedTo": {
                        "ob_id": 8259,
                        "uuid": "535c053640594563ba18f8773f812e86",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Landsat 7 data acquired by Landmap from Infoterra",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Enhanced Thematic Mapper Plus (ETM+); PLATFORMS: Landsat 7; "
                    }
                }
            ]
        },
        {
            "ob_id": 8267,
            "uuid": "c4f5546d08634f59abf11b7fafe27bd8",
            "short_code": "acq",
            "title": "Acquisition Process for: Landsat Mediterranean data acquired by Landmap",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Landsat Thematic Mapper (TM), Enhanced Thematic Mapper Plus (ETM+); PLATFORMS: Landsat 7, Landsat 5; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8250,
                    "uuid": "4894a74f37cb49ea99a6b7d7669228e4",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Landsat 5",
                    "abstract": "Mobile Platform Operation related to the: Landsat 5"
                },
                {
                    "ob_id": 8258,
                    "uuid": "09bcf80950014799ad6e2bdb9ce4a74e",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Landsat 7",
                    "abstract": "Mobile Platform Operation related to the: Landsat 7"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2575,
                    "platform": {
                        "ob_id": 8256,
                        "uuid": "385d8284709749b9a29d33c07670c4fd",
                        "short_code": "plat",
                        "title": "Landsat 7",
                        "abstract": "Landsat 7 was launched as a continuation of the Landsat programme on 15th April 1999 and is still operational as of July 2014. A three-axis attitude control subsystem stabilizes the satellite and keeps the instrument pointed toward Earth to within 0.05 degrees. The LANDSAT World-Wide-Reference system catalogues the worlds land mass into 57,784 scenes, each 115 miles (183 kilometres) wide by 106 miles (170 kilometres) long.\r\n\r\nLaunch date:  15/04/1999\r\nStatus/projected mission lifetime:  5 years +\r\nOrbit parameters:  near circular\r\nNominal altitude:  705 km\r\nOrbit type:\t near-polar, sun-synchronous\r\nInclination:  98.2 degrees\r\nRepeat period:  16 days\r\nEquatorial crossing time:  10.00 local time (descending node)\r\nSwath width:  183 km\r\nResolution:  15 - 60 m \r\nSpecial features:  Panchromatic band, thermal band with 2 gain settings"
                    },
                    "instrument": {
                        "ob_id": 8248,
                        "uuid": "c7d350b1ec99448187607ec46c4ce35e",
                        "short_code": "instr",
                        "title": "Landsat Thematic Mapper (TM)",
                        "abstract": "The Thematic Mapper (TM) is one of the Earth observing sensors introduced in the Landsat program. TMs were placed aboard the Landsat 4 and 5 satellites. The wavelength range for the Thematic Mapper (TM) sensor is from the visible, through the Mid-IR, into the Thermal-IR portion of the electromagnetic spectrum."
                    },
                    "relatedTo": {
                        "ob_id": 8267,
                        "uuid": "c4f5546d08634f59abf11b7fafe27bd8",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Landsat Mediterranean data acquired by Landmap",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Landsat Thematic Mapper (TM), Enhanced Thematic Mapper Plus (ETM+); PLATFORMS: Landsat 7, Landsat 5; "
                    }
                },
                {
                    "ob_id": 2576,
                    "platform": {
                        "ob_id": 8256,
                        "uuid": "385d8284709749b9a29d33c07670c4fd",
                        "short_code": "plat",
                        "title": "Landsat 7",
                        "abstract": "Landsat 7 was launched as a continuation of the Landsat programme on 15th April 1999 and is still operational as of July 2014. A three-axis attitude control subsystem stabilizes the satellite and keeps the instrument pointed toward Earth to within 0.05 degrees. The LANDSAT World-Wide-Reference system catalogues the worlds land mass into 57,784 scenes, each 115 miles (183 kilometres) wide by 106 miles (170 kilometres) long.\r\n\r\nLaunch date:  15/04/1999\r\nStatus/projected mission lifetime:  5 years +\r\nOrbit parameters:  near circular\r\nNominal altitude:  705 km\r\nOrbit type:\t near-polar, sun-synchronous\r\nInclination:  98.2 degrees\r\nRepeat period:  16 days\r\nEquatorial crossing time:  10.00 local time (descending node)\r\nSwath width:  183 km\r\nResolution:  15 - 60 m \r\nSpecial features:  Panchromatic band, thermal band with 2 gain settings"
                    },
                    "instrument": {
                        "ob_id": 8257,
                        "uuid": "dfc450e6a1d54b40b8927c7d0de2de21",
                        "short_code": "instr",
                        "title": "Enhanced Thematic Mapper Plus (ETM+)",
                        "abstract": "The Enhanced Thematic Mapper Plus (ETM+) instrument is a fixed 'whisk-broom', eight-band, multispectral scanning radiometer capable of providing high-resolution imaging information of the Earth's surface onboard Landsat 7. The main improvement from the Landsat 4/5 Thematic Mappers (TMs) is the addition of a panchromatic band with 15 m spatial resolution.\r\nSpectral and spatial characteristics of these bands are shown below.\r\n\r\nBand no. 1\r\nSpectral range .450 to .515 micrometres Ground resolution: 30 m\r\nBand no. 2\r\nSpectral range .525 to .605 micrometres Ground resolution: 30 m\r\nBand no. 3\r\nSpectral range .630 to .690 micrometres Ground resolution: 30 m\r\nBand no. 4\r\nSpectral range .775 to .900 micrometres Ground resolution: 30 m\r\nBand no. 5\r\nSpectral range 1.550 to 1.750 micrometres Ground resolution: 30 m\r\nBand no. 6\r\nSpectral range 10.40 to 12.50 micrometres Ground resolution: 60 m\r\nBand no. 7\r\nSpectral range 2.090 to 2.35 micrometres Ground resolution: 30 m\r\nBand no. 8\r\nSpectral range .520 to .900 micrometres Ground resolution: 15 m"
                    },
                    "relatedTo": {
                        "ob_id": 8267,
                        "uuid": "c4f5546d08634f59abf11b7fafe27bd8",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Landsat Mediterranean data acquired by Landmap",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Landsat Thematic Mapper (TM), Enhanced Thematic Mapper Plus (ETM+); PLATFORMS: Landsat 7, Landsat 5; "
                    }
                },
                {
                    "ob_id": 2577,
                    "platform": {
                        "ob_id": 8246,
                        "uuid": "e9c4a76ba5b64ede82a20d7d69da47a2",
                        "short_code": "plat",
                        "title": "Landsat 5",
                        "abstract": "A nearly identical satellite to Landsat 4, Landsat 5 was launched as part of the Landsat programme in March 1984 and was operational until June 2013. As Landsat 4, it carried Thematic Mapper (TM) and MultiSpectral Scanner (MSS) instruments."
                    },
                    "instrument": {
                        "ob_id": 8248,
                        "uuid": "c7d350b1ec99448187607ec46c4ce35e",
                        "short_code": "instr",
                        "title": "Landsat Thematic Mapper (TM)",
                        "abstract": "The Thematic Mapper (TM) is one of the Earth observing sensors introduced in the Landsat program. TMs were placed aboard the Landsat 4 and 5 satellites. The wavelength range for the Thematic Mapper (TM) sensor is from the visible, through the Mid-IR, into the Thermal-IR portion of the electromagnetic spectrum."
                    },
                    "relatedTo": {
                        "ob_id": 8267,
                        "uuid": "c4f5546d08634f59abf11b7fafe27bd8",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Landsat Mediterranean data acquired by Landmap",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Landsat Thematic Mapper (TM), Enhanced Thematic Mapper Plus (ETM+); PLATFORMS: Landsat 7, Landsat 5; "
                    }
                },
                {
                    "ob_id": 2578,
                    "platform": {
                        "ob_id": 8246,
                        "uuid": "e9c4a76ba5b64ede82a20d7d69da47a2",
                        "short_code": "plat",
                        "title": "Landsat 5",
                        "abstract": "A nearly identical satellite to Landsat 4, Landsat 5 was launched as part of the Landsat programme in March 1984 and was operational until June 2013. As Landsat 4, it carried Thematic Mapper (TM) and MultiSpectral Scanner (MSS) instruments."
                    },
                    "instrument": {
                        "ob_id": 8257,
                        "uuid": "dfc450e6a1d54b40b8927c7d0de2de21",
                        "short_code": "instr",
                        "title": "Enhanced Thematic Mapper Plus (ETM+)",
                        "abstract": "The Enhanced Thematic Mapper Plus (ETM+) instrument is a fixed 'whisk-broom', eight-band, multispectral scanning radiometer capable of providing high-resolution imaging information of the Earth's surface onboard Landsat 7. The main improvement from the Landsat 4/5 Thematic Mappers (TMs) is the addition of a panchromatic band with 15 m spatial resolution.\r\nSpectral and spatial characteristics of these bands are shown below.\r\n\r\nBand no. 1\r\nSpectral range .450 to .515 micrometres Ground resolution: 30 m\r\nBand no. 2\r\nSpectral range .525 to .605 micrometres Ground resolution: 30 m\r\nBand no. 3\r\nSpectral range .630 to .690 micrometres Ground resolution: 30 m\r\nBand no. 4\r\nSpectral range .775 to .900 micrometres Ground resolution: 30 m\r\nBand no. 5\r\nSpectral range 1.550 to 1.750 micrometres Ground resolution: 30 m\r\nBand no. 6\r\nSpectral range 10.40 to 12.50 micrometres Ground resolution: 60 m\r\nBand no. 7\r\nSpectral range 2.090 to 2.35 micrometres Ground resolution: 30 m\r\nBand no. 8\r\nSpectral range .520 to .900 micrometres Ground resolution: 15 m"
                    },
                    "relatedTo": {
                        "ob_id": 8267,
                        "uuid": "c4f5546d08634f59abf11b7fafe27bd8",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Landsat Mediterranean data acquired by Landmap",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Landsat Thematic Mapper (TM), Enhanced Thematic Mapper Plus (ETM+); PLATFORMS: Landsat 7, Landsat 5; "
                    }
                }
            ]
        },
        {
            "ob_id": 8275,
            "uuid": "4432b1d008d242569f7d8bbdbbc0212b",
            "short_code": "acq",
            "title": "Acquisition Process for: Near InfraRed (NIR) red-edge data for Northern Ireland",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Jena Spaceborne Scanner JSS 56; PLATFORMS: RapidEye Satellite Constellation; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8274,
                    "uuid": "23c793bf1a1b47d08da04856adae83c7",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: RapidEye Satellite Constellation",
                    "abstract": "Mobile Platform Operation related to the: RapidEye Satellite Constellation"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2579,
                    "platform": {
                        "ob_id": 8272,
                        "uuid": "dbd1e616e6024f5f9859eac47c9aab19",
                        "short_code": "plat",
                        "title": "RapidEye Satellite Constellation",
                        "abstract": "RapidEye operates a constellation of 5 satellites that are used for spectral imaging, particularly the ‘Red Edge’ band (between red and infrared, 690 to 730nm)."
                    },
                    "instrument": {
                        "ob_id": 8273,
                        "uuid": "afec31bd229c44a79811896aa9170886",
                        "short_code": "instr",
                        "title": "Jena Spaceborne Scanner JSS 56",
                        "abstract": "The Jena Spaceborne Scanner JSS 56 is a pushbroom sensor carried on each RapidEye satellite. Each sensor is capable of collecting image data in five distinct bands of the electromagnetic spectrum; Blue, Green, Red, Red Edge and Near-Infrared (NIR), at 6.5m spatial resolution."
                    },
                    "relatedTo": {
                        "ob_id": 8275,
                        "uuid": "4432b1d008d242569f7d8bbdbbc0212b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Near InfraRed (NIR) red-edge data for Northern Ireland",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Jena Spaceborne Scanner JSS 56; PLATFORMS: RapidEye Satellite Constellation; "
                    }
                }
            ]
        },
        {
            "ob_id": 8283,
            "uuid": "14d30db63bb043cfa8693b8e02c6f556",
            "short_code": "acq",
            "title": "Acquisition Process for: SPOT (Earth-Observing Satellites) Imagery",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: High Resolution Visible Imaging Instrument (HRV); PLATFORMS: SPOT (Earth Observing Satellites) Earth Observation System; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8282,
                    "uuid": "44e6b89f5c0543f6922025522369763a",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: SPOT (Earth Observing Satellites) Earth Observation System",
                    "abstract": "Mobile Platform Operation related to the: SPOT (Earth Observing Satellites) Earth Observation System"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2580,
                    "platform": {
                        "ob_id": 8280,
                        "uuid": "9a7b5ca64f3c4db08492ac1bdad5f934",
                        "short_code": "plat",
                        "title": "SPOT (Earth Observing Satellites) Earth Observation System",
                        "abstract": "There have been 7 SPOT (Satellite Pour l'Observation de la Terre) satellites launched since 1986, providing medium to high resolution of the Earth's surface. SPOT 1, 2 and 3 carried a multi-spectral (XS) and panchromatic (P) sensor on board. SPOT 7 was successfully launched on June 30th 2014. The SPOT satellite Earth Observation System was designed by the Centre National d'Etudes Spatiales (CNES), in France. CNES owns and operates the SPOT satellite system."
                    },
                    "instrument": {
                        "ob_id": 8281,
                        "uuid": "690579323c3044cab6f4cf5ac5d0b8c4",
                        "short_code": "instr",
                        "title": "High Resolution Visible Imaging Instrument (HRV)",
                        "abstract": "The HRV instrument is a multispectral radiometer designed for SPOT (Earth observing satellites) spacecraft. The HRV instrument provides high-resolution imaging in the visible and near-infrared portions of the electromagnetic spectrum. Operating independently of each other, the two HRVs acquire imagery in either multispectral (XS) and/or panchromatic (P) modes at any viewing angle within plus or minus 27 degrees. This off-nadir viewing enables the acquisition of stereoscopic imagery. To make sure the satellite covers every point on the earth's surface, the HRV imaging instruments offer a field of view that is wider than the greatest distance between two adjacent tracks."
                    },
                    "relatedTo": {
                        "ob_id": 8283,
                        "uuid": "14d30db63bb043cfa8693b8e02c6f556",
                        "short_code": "acq",
                        "title": "Acquisition Process for: SPOT (Earth-Observing Satellites) Imagery",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: High Resolution Visible Imaging Instrument (HRV); PLATFORMS: SPOT (Earth Observing Satellites) Earth Observation System; "
                    }
                }
            ]
        },
        {
            "ob_id": 8291,
            "uuid": "57aa7b408fef4feb9b21692539086141",
            "short_code": "acq",
            "title": "Acquisition Process for: TOPSAT (Tactical Operational Satellite) imagery acquired by Landmap",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: Tactical Operational Satellite (TOPSAT); PLATFORMS: Tactical Operational Satellite (TOPSAT); ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8290,
                    "uuid": "df9f847c120449fc8e76e606c97df656",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Tactical Operational Satellite (TOPSAT)",
                    "abstract": "Mobile Platform Operation related to the: Tactical Operational Satellite (TOPSAT)"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2581,
                    "platform": {
                        "ob_id": 8288,
                        "uuid": "45406d2a1eec4ae2a823ccf7245a9876",
                        "short_code": "plat",
                        "title": "Tactical Operational Satellite (TOPSAT)",
                        "abstract": "TOPSAT (Tactical Operational Satellite) is a British Earth observation satellite, launched in October 2005. TOPSAT carries out optical imaging with a ground resolution of 2.5m. TOPSAT was built in the United Kingdom by Surrey Satellite Technology Ltd, QinetiQ and The Rutherford Appleton Laboratory under the British National Space Centre Mosaic programme."
                    },
                    "instrument": {
                        "ob_id": 8289,
                        "uuid": "fe0cc3c8d0884fbab1a58cf20e5452b2",
                        "short_code": "instr",
                        "title": "UNDEFINED instrument associated with platform: Tactical Operational Satellite (TOPSAT)",
                        "abstract": "This instrument is associated with the platform: Tactical Operational Satellite (TOPSAT)"
                    },
                    "relatedTo": {
                        "ob_id": 8291,
                        "uuid": "57aa7b408fef4feb9b21692539086141",
                        "short_code": "acq",
                        "title": "Acquisition Process for: TOPSAT (Tactical Operational Satellite) imagery acquired by Landmap",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: Tactical Operational Satellite (TOPSAT); PLATFORMS: Tactical Operational Satellite (TOPSAT); "
                    }
                }
            ]
        },
        {
            "ob_id": 8302,
            "uuid": "747d50622dc5490fbe04b65343158a33",
            "short_code": "acq",
            "title": "Acquisition Process for: Level 1C data from the IASI (Infrared Atmospheric Sounding Interferometer) Instrument on board the MetOp-B satellite.",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: IASI; PLATFORMS: Metop-B; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8301,
                    "uuid": "d1d4ffcf747d4e95a3614aa20f1855da",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Metop-B",
                    "abstract": "Mobile Platform Operation related to the: Metop-B"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2582,
                    "platform": {
                        "ob_id": 8299,
                        "uuid": "84a6355ac58249cc8c636e77a243c86a",
                        "short_code": "plat",
                        "title": "Metop-B",
                        "abstract": "Metop-B, launched on the 17th September 2012, is the second in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS)."
                    },
                    "instrument": {
                        "ob_id": 8300,
                        "uuid": "57fc4dbabdf0434b9584836acac24ffe",
                        "short_code": "instr",
                        "title": "IASI",
                        "abstract": "Data from the IASI instruments on board the Eumetsat EPS MetOp satellite series. The Infrared Atmospheric Sounding Interferometer (IASI) is designed to measure the infrared spectrum emitted by the earth. IASI provides infrared soundings of the temperature profiles in the troposphere and lower stratosphere, moisture profiles in the troposphere, as well as some of the chemical components playing a key role in the climate monitoring, global change and atmospheric chemistry."
                    },
                    "relatedTo": {
                        "ob_id": 8302,
                        "uuid": "747d50622dc5490fbe04b65343158a33",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Level 1C data from the IASI (Infrared Atmospheric Sounding Interferometer) Instrument on board the MetOp-B satellite.",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: IASI; PLATFORMS: Metop-B; "
                    }
                }
            ]
        },
        {
            "ob_id": 8308,
            "uuid": "4b3bf76b9a4e4405afd10a639f6dc8b3",
            "short_code": "acq",
            "title": "Acquisition Process for: Level 2 data from the IASI (Infrared Atmospheric Sounding Interferometer) instrument on board the Metop-B satellite",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: IASI; PLATFORMS: Metop-B; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8301,
                    "uuid": "d1d4ffcf747d4e95a3614aa20f1855da",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Metop-B",
                    "abstract": "Mobile Platform Operation related to the: Metop-B"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2583,
                    "platform": {
                        "ob_id": 8299,
                        "uuid": "84a6355ac58249cc8c636e77a243c86a",
                        "short_code": "plat",
                        "title": "Metop-B",
                        "abstract": "Metop-B, launched on the 17th September 2012, is the second in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS)."
                    },
                    "instrument": {
                        "ob_id": 8300,
                        "uuid": "57fc4dbabdf0434b9584836acac24ffe",
                        "short_code": "instr",
                        "title": "IASI",
                        "abstract": "Data from the IASI instruments on board the Eumetsat EPS MetOp satellite series. The Infrared Atmospheric Sounding Interferometer (IASI) is designed to measure the infrared spectrum emitted by the earth. IASI provides infrared soundings of the temperature profiles in the troposphere and lower stratosphere, moisture profiles in the troposphere, as well as some of the chemical components playing a key role in the climate monitoring, global change and atmospheric chemistry."
                    },
                    "relatedTo": {
                        "ob_id": 8308,
                        "uuid": "4b3bf76b9a4e4405afd10a639f6dc8b3",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Level 2 data from the IASI (Infrared Atmospheric Sounding Interferometer) instrument on board the Metop-B satellite",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: IASI; PLATFORMS: Metop-B; "
                    }
                }
            ]
        },
        {
            "ob_id": 8316,
            "uuid": "d971efd5cd7a40d399e020fbb774a237",
            "short_code": "acq",
            "title": "Acquisition Process for: (A)ATSR Validation Campaign - SISTeR SST Data from RMS Queen Mary 2",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Scanning Infrared Sea surface Temperature Radiometer (SISTeR); PLATFORMS: RMS Queen Mary 2; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8315,
                    "uuid": "dfc68b4a51354170945d0d01cad50413",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: RMS Queen Mary 2",
                    "abstract": "Mobile Platform Operation related to the: RMS Queen Mary 2"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2584,
                    "platform": {
                        "ob_id": 8313,
                        "uuid": "9bd4d6a9d8f34976931d76c1b200f478",
                        "short_code": "plat",
                        "title": "RMS Queen Mary 2",
                        "abstract": "The ocean liner RMS Queen Mary 2 is used as a platform for Scanning Infrared Sea surface Temperature Radiometer (SISTeR), rain gauge and GPS antenna, which has collected SST data since 2010 for satellite validation. RMS Queen Mary offers global-wide coverage which includes the Atlantic Ocean, Indian Ocean and the Western Pacific."
                    },
                    "instrument": {
                        "ob_id": 8314,
                        "uuid": "25b1705e401a42509e63cf38404ec894",
                        "short_code": "instr",
                        "title": "Scanning Infrared Sea surface Temperature Radiometer (SISTeR)",
                        "abstract": "The Scanning Infrared Sea surface Temperature Radiometer (SISTeR), developed at Rutherford Appleton Laboratory, is a self-calibrating filter radiometer for the in situ measurement of skin SST, that has been used to validate the radiometers ATSR-1, ATSR-2, AATSR and SLSTR which were on-board ERS-1, ERS-2 ENVISAT and Sentinel-3 respectively. The self-calibration involves the use of two internal reference blackbodies. The filters used are 3.7 microns, 10.8 microns and 12.0 microns. The instrument has been deployed on MS Color Festival (2006), MS Prinsessa Ragnhild (2008), and RMS Queen Mary 2 (2010-present)."
                    },
                    "relatedTo": {
                        "ob_id": 8316,
                        "uuid": "d971efd5cd7a40d399e020fbb774a237",
                        "short_code": "acq",
                        "title": "Acquisition Process for: (A)ATSR Validation Campaign - SISTeR SST Data from RMS Queen Mary 2",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Scanning Infrared Sea surface Temperature Radiometer (SISTeR); PLATFORMS: RMS Queen Mary 2; "
                    }
                }
            ]
        },
        {
            "ob_id": 8321,
            "uuid": "3b7615e66e09457bab8d6245b9df540d",
            "short_code": "acq",
            "title": "Acquisition Process for: (A)ATSR Validation Campaign - SISTeR SST Data from MS Prinsesse Ragnhild",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Scanning Infrared Sea surface Temperature Radiometer (SISTeR); PLATFORMS: MS Prinsesse Ragnhild; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8320,
                    "uuid": "962049ec4dad46bfa234b9944acd5ce9",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: MS Prinsesse Ragnhild",
                    "abstract": "Mobile Platform Operation related to the: MS Prinsesse Ragnhild"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2585,
                    "platform": {
                        "ob_id": 8319,
                        "uuid": "116d6c622c8a499b856135c7296a99a1",
                        "short_code": "plat",
                        "title": "MS Prinsesse Ragnhild",
                        "abstract": "MS Prinsesse Ragnhild is a cruiseferry which carried Scanning Infrared Sea surface Temperature Radiometer (SISTeR), rain gauge and GPS antenna, to measure SST in 2006 to be used for the (A)ATSR Validation Campaign. The cruiseferry travelled in the North Sea during the period."
                    },
                    "instrument": {
                        "ob_id": 8314,
                        "uuid": "25b1705e401a42509e63cf38404ec894",
                        "short_code": "instr",
                        "title": "Scanning Infrared Sea surface Temperature Radiometer (SISTeR)",
                        "abstract": "The Scanning Infrared Sea surface Temperature Radiometer (SISTeR), developed at Rutherford Appleton Laboratory, is a self-calibrating filter radiometer for the in situ measurement of skin SST, that has been used to validate the radiometers ATSR-1, ATSR-2, AATSR and SLSTR which were on-board ERS-1, ERS-2 ENVISAT and Sentinel-3 respectively. The self-calibration involves the use of two internal reference blackbodies. The filters used are 3.7 microns, 10.8 microns and 12.0 microns. The instrument has been deployed on MS Color Festival (2006), MS Prinsessa Ragnhild (2008), and RMS Queen Mary 2 (2010-present)."
                    },
                    "relatedTo": {
                        "ob_id": 8321,
                        "uuid": "3b7615e66e09457bab8d6245b9df540d",
                        "short_code": "acq",
                        "title": "Acquisition Process for: (A)ATSR Validation Campaign - SISTeR SST Data from MS Prinsesse Ragnhild",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Scanning Infrared Sea surface Temperature Radiometer (SISTeR); PLATFORMS: MS Prinsesse Ragnhild; "
                    }
                }
            ]
        },
        {
            "ob_id": 8326,
            "uuid": "bf30da00a318433fb9ca3ed14b523388",
            "short_code": "acq",
            "title": "Acquisition Process for: (A)ATSR Validation Campaign - SISTeR SST Data from MS Color Festival",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Scanning Infrared Sea surface Temperature Radiometer (SISTeR); PLATFORMS: MS Color Festival; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8325,
                    "uuid": "14da6d4d0c444e56a4cbf86843b7901a",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: MS Color Festival",
                    "abstract": "Mobile Platform Operation related to the: MS Color Festival"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2586,
                    "platform": {
                        "ob_id": 8324,
                        "uuid": "f5f1a61db070486b82f9de5899eaa492",
                        "short_code": "plat",
                        "title": "MS Color Festival",
                        "abstract": "MS Color Festival is a cruiseferry which carried Scanning Infrared Sea surface Temperature Radiometer (SISTeR), rain gauge and GPS antenna, to measure SST in 2006 to be used for the (A)ATSR Validation Campaign. The cruiseferry travelled between Oslo, Norway and Frederikshavn, Denmark during the period."
                    },
                    "instrument": {
                        "ob_id": 8314,
                        "uuid": "25b1705e401a42509e63cf38404ec894",
                        "short_code": "instr",
                        "title": "Scanning Infrared Sea surface Temperature Radiometer (SISTeR)",
                        "abstract": "The Scanning Infrared Sea surface Temperature Radiometer (SISTeR), developed at Rutherford Appleton Laboratory, is a self-calibrating filter radiometer for the in situ measurement of skin SST, that has been used to validate the radiometers ATSR-1, ATSR-2, AATSR and SLSTR which were on-board ERS-1, ERS-2 ENVISAT and Sentinel-3 respectively. The self-calibration involves the use of two internal reference blackbodies. The filters used are 3.7 microns, 10.8 microns and 12.0 microns. The instrument has been deployed on MS Color Festival (2006), MS Prinsessa Ragnhild (2008), and RMS Queen Mary 2 (2010-present)."
                    },
                    "relatedTo": {
                        "ob_id": 8326,
                        "uuid": "bf30da00a318433fb9ca3ed14b523388",
                        "short_code": "acq",
                        "title": "Acquisition Process for: (A)ATSR Validation Campaign - SISTeR SST Data from MS Color Festival",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Scanning Infrared Sea surface Temperature Radiometer (SISTeR); PLATFORMS: MS Color Festival; "
                    }
                }
            ]
        },
        {
            "ob_id": 8336,
            "uuid": "9402aba50f6144b383b8ffcd721a4860",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from LANDSAT7 ETMPLUS at Landsat7 for the Landsat Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: LANDSAT7 ETMPLUS; PLATFORMS: Landsat7; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 7865,
                    "uuid": "9b214516190a4fea9dc01668679f510d",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Landsat7",
                    "abstract": "Mobile Platform Operation related to the: Landsat7"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2587,
                    "platform": {
                        "ob_id": 7863,
                        "uuid": "3ee22191b6d749d68bc09af9fb230c35",
                        "short_code": "plat",
                        "title": "Landsat7",
                        "abstract": "Landsat7 is the satellite on which the ETM+ instrument is mounted.  Landsat7 is placed in a 16 day repeat polar orbit and was launched in 1999."
                    },
                    "instrument": {
                        "ob_id": 7864,
                        "uuid": "f51158da62d343c59d43f5216c610297",
                        "short_code": "instr",
                        "title": "LANDSAT7 ETMPLUS",
                        "abstract": "The ETM+ (extended thematic mapper) sensor is an eight band nadir-viewing, multi-spectral scanning radiometer providing high-resolution images of the earth, detecting visible, near-infrared, short wave and thermal infrared frequency bands.\r\nSpectral and spatial characteristics of these bands are shown below.\r\n\r\nBand no. 1\r\nSpectral range .450 to .515 micrometres  Ground resolution: 30 m\r\nBand no. 2\r\nSpectral range .525 to .605 micrometres  Ground resolution: 30 m\r\nBand no. 3\r\nSpectral range .630 to .690 micrometres  Ground resolution: 30 m\r\nBand no. 4\r\nSpectral range .775 to .900 micrometres  Ground resolution: 30 m\r\nBand no. 5\r\nSpectral range 1.550 to 1.750 micrometres  Ground resolution: 30 m\r\nBand no. 6\r\nSpectral range 10.40 to 12.50 micrometres  Ground resolution: 60 m\r\nBand no. 7\r\nSpectral range 2.090 to 2.35 micrometres  Ground resolution: 30 m\r\nBand no. 8\r\nSpectral range .520 to .900 micrometres  Ground resolution: 15 m\r\n"
                    },
                    "relatedTo": {
                        "ob_id": 8336,
                        "uuid": "9402aba50f6144b383b8ffcd721a4860",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from LANDSAT7 ETMPLUS at Landsat7 for the Landsat Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: LANDSAT7 ETMPLUS; PLATFORMS: Landsat7; "
                    }
                }
            ]
        },
        {
            "ob_id": 8344,
            "uuid": "c1311786388a421fa0675d8b69258757",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Envisat - MERIS at Envisat for the MEdium Resolution Imaging Spectrometer (MERIS) Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Envisat - MERIS; 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": 2588,
                    "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": 8342,
                        "uuid": "ac18e088c2ad4c088396ac97e177e6aa",
                        "short_code": "instr",
                        "title": "Envisat - MERIS",
                        "abstract": "The Medium Resolution Imaging Spectrometer (MERIS) is one of the ten instruments onboard the Envisat satellite launched on the 28th of February 2002 from Kourou (French Guyana) and operated by the European Space Agency (ESA)."
                    },
                    "relatedTo": {
                        "ob_id": 8344,
                        "uuid": "c1311786388a421fa0675d8b69258757",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Envisat - MERIS at Envisat for the MEdium Resolution Imaging Spectrometer (MERIS) Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Envisat - MERIS; PLATFORMS: Envisat; "
                    }
                }
            ]
        },
        {
            "ob_id": 8354,
            "uuid": "592ed6b3b3504ed2849b977adf12bd2f",
            "short_code": "acq",
            "title": "Acquisition Process for: CALIPSO Lidar Level 2 5km Cloud Layer Version 3-30 Product (CAL_LID_L2_05kmCLay-Prov-V3-30)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8353,
                    "uuid": "0f8a8261419a4e9e94f72fc62456092b",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                    "abstract": "Mobile Platform Operation related to the: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2589,
                    "platform": {
                        "ob_id": 8351,
                        "uuid": "8be6f5d13183411c905984e976dcb0a9",
                        "short_code": "plat",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                        "abstract": "CALIPSO is a Franco-American satellite launched in 2006, with a specific purpose of advanced measurement of cloud and aerosols. The satellite is a part of the Afternoon Constellation (A-Train) under NASA-centred Earth Observation System (EOS). A-Train is a group of polar orbiting satellites following closely with each other for synergetic measurements. They pass through the  the equator around 13:00 and 01:00. CALIPSO is the first satellite that is able to provide data of vertical profiles of aerosol. These data is used for studying direct and indirect aerosol forcings. Vertical cloud profile is also required to predict precipitation and the strength of the circulation. The satellite contains Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP), Wide Field Camera (WFC) and Imaging Infrared Radiometer (IIR)."
                    },
                    "instrument": {
                        "ob_id": 8352,
                        "uuid": "7fd40aaed5aa488fad251a98b40357a5",
                        "short_code": "instr",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP)",
                        "abstract": "The Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP) is a two-wavelength polarisation-sensitive lidar which creates high-resolution vertical profiles of cloud and aerosol. The lidar uses 1064 nm to measure backscatter intesity, and two channels measuring orthogonally polarised components of the 532 nm backscatter signal."
                    },
                    "relatedTo": {
                        "ob_id": 8354,
                        "uuid": "592ed6b3b3504ed2849b977adf12bd2f",
                        "short_code": "acq",
                        "title": "Acquisition Process for: CALIPSO Lidar Level 2 5km Cloud Layer Version 3-30 Product (CAL_LID_L2_05kmCLay-Prov-V3-30)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 8360,
            "uuid": "964edc04d5204d74abfc330ec2abcea6",
            "short_code": "acq",
            "title": "Acquisition Process for: CALIPSO Lidar Level 2 Vertical Feature Mask Version 3-01 Product (CAL_LID_L2_VFM-ValStage1-V3-01)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8353,
                    "uuid": "0f8a8261419a4e9e94f72fc62456092b",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                    "abstract": "Mobile Platform Operation related to the: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2590,
                    "platform": {
                        "ob_id": 8351,
                        "uuid": "8be6f5d13183411c905984e976dcb0a9",
                        "short_code": "plat",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                        "abstract": "CALIPSO is a Franco-American satellite launched in 2006, with a specific purpose of advanced measurement of cloud and aerosols. The satellite is a part of the Afternoon Constellation (A-Train) under NASA-centred Earth Observation System (EOS). A-Train is a group of polar orbiting satellites following closely with each other for synergetic measurements. They pass through the  the equator around 13:00 and 01:00. CALIPSO is the first satellite that is able to provide data of vertical profiles of aerosol. These data is used for studying direct and indirect aerosol forcings. Vertical cloud profile is also required to predict precipitation and the strength of the circulation. The satellite contains Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP), Wide Field Camera (WFC) and Imaging Infrared Radiometer (IIR)."
                    },
                    "instrument": {
                        "ob_id": 8352,
                        "uuid": "7fd40aaed5aa488fad251a98b40357a5",
                        "short_code": "instr",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP)",
                        "abstract": "The Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP) is a two-wavelength polarisation-sensitive lidar which creates high-resolution vertical profiles of cloud and aerosol. The lidar uses 1064 nm to measure backscatter intesity, and two channels measuring orthogonally polarised components of the 532 nm backscatter signal."
                    },
                    "relatedTo": {
                        "ob_id": 8360,
                        "uuid": "964edc04d5204d74abfc330ec2abcea6",
                        "short_code": "acq",
                        "title": "Acquisition Process for: CALIPSO Lidar Level 2 Vertical Feature Mask Version 3-01 Product (CAL_LID_L2_VFM-ValStage1-V3-01)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 8365,
            "uuid": "ac0e2d2be32a462da556befd2ca3c827",
            "short_code": "acq",
            "title": "Acquisition Process for: CALIPSO Lidar Level 2 Aerosol Profile Version 3-01 Product (CAL_LID_L2_05kmAPro-Prov-V3-01)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8353,
                    "uuid": "0f8a8261419a4e9e94f72fc62456092b",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                    "abstract": "Mobile Platform Operation related to the: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2591,
                    "platform": {
                        "ob_id": 8351,
                        "uuid": "8be6f5d13183411c905984e976dcb0a9",
                        "short_code": "plat",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                        "abstract": "CALIPSO is a Franco-American satellite launched in 2006, with a specific purpose of advanced measurement of cloud and aerosols. The satellite is a part of the Afternoon Constellation (A-Train) under NASA-centred Earth Observation System (EOS). A-Train is a group of polar orbiting satellites following closely with each other for synergetic measurements. They pass through the  the equator around 13:00 and 01:00. CALIPSO is the first satellite that is able to provide data of vertical profiles of aerosol. These data is used for studying direct and indirect aerosol forcings. Vertical cloud profile is also required to predict precipitation and the strength of the circulation. The satellite contains Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP), Wide Field Camera (WFC) and Imaging Infrared Radiometer (IIR)."
                    },
                    "instrument": {
                        "ob_id": 8352,
                        "uuid": "7fd40aaed5aa488fad251a98b40357a5",
                        "short_code": "instr",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP)",
                        "abstract": "The Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP) is a two-wavelength polarisation-sensitive lidar which creates high-resolution vertical profiles of cloud and aerosol. The lidar uses 1064 nm to measure backscatter intesity, and two channels measuring orthogonally polarised components of the 532 nm backscatter signal."
                    },
                    "relatedTo": {
                        "ob_id": 8365,
                        "uuid": "ac0e2d2be32a462da556befd2ca3c827",
                        "short_code": "acq",
                        "title": "Acquisition Process for: CALIPSO Lidar Level 2 Aerosol Profile Version 3-01 Product (CAL_LID_L2_05kmAPro-Prov-V3-01)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 8370,
            "uuid": "92e1dbeb0dcf43fd8c0d8fb2227e1fac",
            "short_code": "acq",
            "title": "Acquisition Process for: CALIPSO Lidar Level 1B Version 3-30 Product (CAL_LID_L1-ValStage1-V3-30)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8353,
                    "uuid": "0f8a8261419a4e9e94f72fc62456092b",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                    "abstract": "Mobile Platform Operation related to the: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2592,
                    "platform": {
                        "ob_id": 8351,
                        "uuid": "8be6f5d13183411c905984e976dcb0a9",
                        "short_code": "plat",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                        "abstract": "CALIPSO is a Franco-American satellite launched in 2006, with a specific purpose of advanced measurement of cloud and aerosols. The satellite is a part of the Afternoon Constellation (A-Train) under NASA-centred Earth Observation System (EOS). A-Train is a group of polar orbiting satellites following closely with each other for synergetic measurements. They pass through the  the equator around 13:00 and 01:00. CALIPSO is the first satellite that is able to provide data of vertical profiles of aerosol. These data is used for studying direct and indirect aerosol forcings. Vertical cloud profile is also required to predict precipitation and the strength of the circulation. The satellite contains Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP), Wide Field Camera (WFC) and Imaging Infrared Radiometer (IIR)."
                    },
                    "instrument": {
                        "ob_id": 8352,
                        "uuid": "7fd40aaed5aa488fad251a98b40357a5",
                        "short_code": "instr",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP)",
                        "abstract": "The Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP) is a two-wavelength polarisation-sensitive lidar which creates high-resolution vertical profiles of cloud and aerosol. The lidar uses 1064 nm to measure backscatter intesity, and two channels measuring orthogonally polarised components of the 532 nm backscatter signal."
                    },
                    "relatedTo": {
                        "ob_id": 8370,
                        "uuid": "92e1dbeb0dcf43fd8c0d8fb2227e1fac",
                        "short_code": "acq",
                        "title": "Acquisition Process for: CALIPSO Lidar Level 1B Version 3-30 Product (CAL_LID_L1-ValStage1-V3-30)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 8375,
            "uuid": "31726818a47f4ae59c5ca000d1f6deac",
            "short_code": "acq",
            "title": "Acquisition Process for: CALIPSO Lidar Level 2 5km Cloud Layer Version 3-02 Product (CAL_LID_L2_05kmCLay-Prov-V3-02)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8353,
                    "uuid": "0f8a8261419a4e9e94f72fc62456092b",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                    "abstract": "Mobile Platform Operation related to the: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2593,
                    "platform": {
                        "ob_id": 8351,
                        "uuid": "8be6f5d13183411c905984e976dcb0a9",
                        "short_code": "plat",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
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                        "short_code": "acq",
                        "title": "Acquisition Process for: CALIPSO Lidar Level 2 Vertical Feature Mask Version 3-02 Product (CAL_LID_L2_VFM-ValStage1-V3-02)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 8415,
            "uuid": "52e49fc8bac94b48b3d18a3434ce0492",
            "short_code": "acq",
            "title": "Acquisition Process for: CALIPSO Lidar Level 2 5km Cloud Layer Version 3-01 Product (CAL_LID_L2_05kmCLay-Prov-V3-01)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8353,
                    "uuid": "0f8a8261419a4e9e94f72fc62456092b",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                    "abstract": "Mobile Platform Operation related to the: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2601,
                    "platform": {
                        "ob_id": 8351,
                        "uuid": "8be6f5d13183411c905984e976dcb0a9",
                        "short_code": "plat",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                        "abstract": "CALIPSO is a Franco-American satellite launched in 2006, with a specific purpose of advanced measurement of cloud and aerosols. The satellite is a part of the Afternoon Constellation (A-Train) under NASA-centred Earth Observation System (EOS). A-Train is a group of polar orbiting satellites following closely with each other for synergetic measurements. They pass through the  the equator around 13:00 and 01:00. CALIPSO is the first satellite that is able to provide data of vertical profiles of aerosol. These data is used for studying direct and indirect aerosol forcings. Vertical cloud profile is also required to predict precipitation and the strength of the circulation. The satellite contains Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP), Wide Field Camera (WFC) and Imaging Infrared Radiometer (IIR)."
                    },
                    "instrument": {
                        "ob_id": 8352,
                        "uuid": "7fd40aaed5aa488fad251a98b40357a5",
                        "short_code": "instr",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP)",
                        "abstract": "The Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP) is a two-wavelength polarisation-sensitive lidar which creates high-resolution vertical profiles of cloud and aerosol. The lidar uses 1064 nm to measure backscatter intesity, and two channels measuring orthogonally polarised components of the 532 nm backscatter signal."
                    },
                    "relatedTo": {
                        "ob_id": 8415,
                        "uuid": "52e49fc8bac94b48b3d18a3434ce0492",
                        "short_code": "acq",
                        "title": "Acquisition Process for: CALIPSO Lidar Level 2 5km Cloud Layer Version 3-01 Product (CAL_LID_L2_05kmCLay-Prov-V3-01)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 8420,
            "uuid": "0a43ba92f0944793a79f650e814e6e8b",
            "short_code": "acq",
            "title": "Acquisition Process for: CALIPSO Lidar Level 2 1km Cloud Layer Version 3-30 Product (CAL_LID_L2_01kmCLay-ValStage1-V3-30)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8353,
                    "uuid": "0f8a8261419a4e9e94f72fc62456092b",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                    "abstract": "Mobile Platform Operation related to the: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2602,
                    "platform": {
                        "ob_id": 8351,
                        "uuid": "8be6f5d13183411c905984e976dcb0a9",
                        "short_code": "plat",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                        "abstract": "CALIPSO is a Franco-American satellite launched in 2006, with a specific purpose of advanced measurement of cloud and aerosols. The satellite is a part of the Afternoon Constellation (A-Train) under NASA-centred Earth Observation System (EOS). A-Train is a group of polar orbiting satellites following closely with each other for synergetic measurements. They pass through the  the equator around 13:00 and 01:00. CALIPSO is the first satellite that is able to provide data of vertical profiles of aerosol. These data is used for studying direct and indirect aerosol forcings. Vertical cloud profile is also required to predict precipitation and the strength of the circulation. The satellite contains Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP), Wide Field Camera (WFC) and Imaging Infrared Radiometer (IIR)."
                    },
                    "instrument": {
                        "ob_id": 8352,
                        "uuid": "7fd40aaed5aa488fad251a98b40357a5",
                        "short_code": "instr",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP)",
                        "abstract": "The Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP) is a two-wavelength polarisation-sensitive lidar which creates high-resolution vertical profiles of cloud and aerosol. The lidar uses 1064 nm to measure backscatter intesity, and two channels measuring orthogonally polarised components of the 532 nm backscatter signal."
                    },
                    "relatedTo": {
                        "ob_id": 8420,
                        "uuid": "0a43ba92f0944793a79f650e814e6e8b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: CALIPSO Lidar Level 2 1km Cloud Layer Version 3-30 Product (CAL_LID_L2_01kmCLay-ValStage1-V3-30)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 8425,
            "uuid": "27d1e9aa922f4a7cadb2ca5b45465025",
            "short_code": "acq",
            "title": "Acquisition Process for: CALIPSO Lidar Level 2 1km Cloud Layer Version 3-02 Product (CAL_LID_L2_01kmCLay-ValStage1-V3-02)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8353,
                    "uuid": "0f8a8261419a4e9e94f72fc62456092b",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                    "abstract": "Mobile Platform Operation related to the: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2603,
                    "platform": {
                        "ob_id": 8351,
                        "uuid": "8be6f5d13183411c905984e976dcb0a9",
                        "short_code": "plat",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite",
                        "abstract": "CALIPSO is a Franco-American satellite launched in 2006, with a specific purpose of advanced measurement of cloud and aerosols. The satellite is a part of the Afternoon Constellation (A-Train) under NASA-centred Earth Observation System (EOS). A-Train is a group of polar orbiting satellites following closely with each other for synergetic measurements. They pass through the  the equator around 13:00 and 01:00. CALIPSO is the first satellite that is able to provide data of vertical profiles of aerosol. These data is used for studying direct and indirect aerosol forcings. Vertical cloud profile is also required to predict precipitation and the strength of the circulation. The satellite contains Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP), Wide Field Camera (WFC) and Imaging Infrared Radiometer (IIR)."
                    },
                    "instrument": {
                        "ob_id": 8352,
                        "uuid": "7fd40aaed5aa488fad251a98b40357a5",
                        "short_code": "instr",
                        "title": "Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP)",
                        "abstract": "The Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP) is a two-wavelength polarisation-sensitive lidar which creates high-resolution vertical profiles of cloud and aerosol. The lidar uses 1064 nm to measure backscatter intesity, and two channels measuring orthogonally polarised components of the 532 nm backscatter signal."
                    },
                    "relatedTo": {
                        "ob_id": 8425,
                        "uuid": "27d1e9aa922f4a7cadb2ca5b45465025",
                        "short_code": "acq",
                        "title": "Acquisition Process for: CALIPSO Lidar Level 2 1km Cloud Layer Version 3-02 Product (CAL_LID_L2_01kmCLay-ValStage1-V3-02)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Cloud-Aerosol Lidar with Orthogonal Polarization (CALIOP); PLATFORMS: Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observation (CALIPSO) Satellite; "
                    }
                }
            ]
        },
        {
            "ob_id": 8434,
            "uuid": "f180256078ab4930bebaa55adca36310",
            "short_code": "acq",
            "title": "Acquisition Process for: Advanced Very High Resolution Radiometer (AVHRR) Global Area Coverage (GAC) Level 1B data",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Advanced Very High Resolution Radiometer (AVHRR); PLATFORMS: NOAA Polar Orbiting environmental satellites (POES), Metop-A, Metop-B; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8301,
                    "uuid": "d1d4ffcf747d4e95a3614aa20f1855da",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Metop-B",
                    "abstract": "Mobile Platform Operation related to the: Metop-B"
                },
                {
                    "ob_id": 8209,
                    "uuid": "f0f061d64cca41c3a4221b713fd6b1be",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Metop-A",
                    "abstract": "Mobile Platform Operation related to the: Metop-A"
                },
                {
                    "ob_id": 8,
                    "uuid": "110154772fc04bdf8029022b40e19521",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: NOAA Polar Orbiting environmental satellites (POES)",
                    "abstract": "The Polar Orbiting Environmental satellites consist of a polar orbiter series of satellites from TIROS-N, NOAA-6 through NOAA-14. The POES system includes the Advanced Very High Resolution Radiometer (AVHRR) and the Tiros Operational Vertical Sounder (TOVS).\r\n\r\nThe Polar Orbiting Environmental series of satellites commenced with TIROS-N (launched in October 1978) and continued with NOAA-A (launched in June 1979 and renamed NOAA-6), NOAA-C (launched in June 1981 and renamed NOAA-7), NOAA-E (launched in March 1983 and renamed NOAA-8), NOAA-F (launched in December 1984 and renamed NOAA-9), NOAA-G (launched in September 1986 and renamed NOAA-10), NOAA-H (launched in September 1988 and renamed NOAA-11), NOAA-D (launched in May 1991 and renamed NOAA-12), NOAA-I (launched in August 1993 and renamed NOAA-13) and NOAA-J (launched in December 1994 and renamed NOAA-14).\r\n\r\nThe POES satellite system offers the advantage of daily global coverage, by making nearly polar orbits roughly 14.1 times daily. Since the number of orbits per day is not an integer the sub orbital tracks do not repeat on a daily basis, although the local solar time of each satellite's passage is essentially unchanged for any latitude. The POES system includes the Advanced Very High Resolution Radiometer (AVHRR) and the Tiros Operational Vertical Sounder (TOVS).\r\n\r\nBecause of the polar orbiting nature of the POES series satellites, these satellites are able to collect global data on a daily basis for a variety of land, ocean, and atmospheric applications. Data from the POES series supports a broad range of environmental monitoring applications including weather analysis and forecasting, climate research and prediction, global sea surface temperature measurements, atmospheric soundings of temperature and humidity, ocean dynamics research, volcanic eruption monitoring, forest fire detection, global vegetation analysis, search and rescue, and many other applications."
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2604,
                    "platform": {
                        "ob_id": 6,
                        "uuid": "edbc618730c043a383b8fa9b8200cfb6",
                        "short_code": "plat",
                        "title": "NOAA Polar Orbiting environmental satellites (POES)",
                        "abstract": "The Polar Orbiting Environmental satellites consist of a polar orbiter series of satellites from TIROS-N, NOAA-6 through NOAA-14. The POES system includes the Advanced Very High Resolution Radiometer (AVHRR) and the Tiros Operational Vertical Sounder (TOVS)."
                    },
                    "instrument": {
                        "ob_id": 1665,
                        "uuid": "65564b1bbd5c4d76aa0638adb40fbcc8",
                        "short_code": "instr",
                        "title": "Advanced Very High Resolution Radiometer (AVHRR)",
                        "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": 8434,
                        "uuid": "f180256078ab4930bebaa55adca36310",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Advanced Very High Resolution Radiometer (AVHRR) Global Area Coverage (GAC) Level 1B data",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Advanced Very High Resolution Radiometer (AVHRR); PLATFORMS: NOAA Polar Orbiting environmental satellites (POES), Metop-A, Metop-B; "
                    }
                },
                {
                    "ob_id": 2605,
                    "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": 1665,
                        "uuid": "65564b1bbd5c4d76aa0638adb40fbcc8",
                        "short_code": "instr",
                        "title": "Advanced Very High Resolution Radiometer (AVHRR)",
                        "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": 8434,
                        "uuid": "f180256078ab4930bebaa55adca36310",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Advanced Very High Resolution Radiometer (AVHRR) Global Area Coverage (GAC) Level 1B data",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Advanced Very High Resolution Radiometer (AVHRR); PLATFORMS: NOAA Polar Orbiting environmental satellites (POES), Metop-A, Metop-B; "
                    }
                },
                {
                    "ob_id": 2606,
                    "platform": {
                        "ob_id": 8299,
                        "uuid": "84a6355ac58249cc8c636e77a243c86a",
                        "short_code": "plat",
                        "title": "Metop-B",
                        "abstract": "Metop-B, launched on the 17th September 2012, is the second in a series of three satellites forming the space segment of the EUMETSAT Polar System (EPS)."
                    },
                    "instrument": {
                        "ob_id": 1665,
                        "uuid": "65564b1bbd5c4d76aa0638adb40fbcc8",
                        "short_code": "instr",
                        "title": "Advanced Very High Resolution Radiometer (AVHRR)",
                        "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": 8434,
                        "uuid": "f180256078ab4930bebaa55adca36310",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Advanced Very High Resolution Radiometer (AVHRR) Global Area Coverage (GAC) Level 1B data",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Advanced Very High Resolution Radiometer (AVHRR); PLATFORMS: NOAA Polar Orbiting environmental satellites (POES), Metop-A, Metop-B; "
                    }
                }
            ]
        },
        {
            "ob_id": 8453,
            "uuid": "bb890e4dd33645689c6fc769d9c1dc8f",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from AVHRR series at NOAA polar orbiting satellites for the NOAA Polar Orbiting Satellite Series Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: AVHRR series; PLATFORMS: NOAA polar orbiting satellites; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8452,
                    "uuid": "c0c56ccaf7e0407b91517d2085072fbc",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: NOAA polar orbiting satellites",
                    "abstract": "Mobile Platform Operation related to the: NOAA polar orbiting satellites"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2607,
                    "platform": {
                        "ob_id": 8450,
                        "uuid": "5b79fd8c19974b38b90174eafbfd5887",
                        "short_code": "plat",
                        "title": "NOAA polar orbiting satellites",
                        "abstract": "The NOAA Polar Orbiter series of satellites includes the TIROS-N, NOAA-6 through NOAA-14 polar orbiters."
                    },
                    "instrument": {
                        "ob_id": 8451,
                        "uuid": "a78c6eb7196f42c7a482317ebe638758",
                        "short_code": "instr",
                        "title": "AVHRR series",
                        "abstract": "The Advanced Very High Resolution Radiometer (AVHRR) sensor is a broad-band, 4- or 5- channel scanning radiometer, sensing in the visible, near-infrared, and thermal infrared. Its objective is to provide radiance data for investigation of clouds, land-water boundaries, snow and ice extent, ice or snow melt inception, day and night cloud distribution, temperatures of radiating surfaces, and sea surface temperature. Other applications include agricultural assessment, land cover mapping, production of large-area maps, and evaluation of regional and continental snow cover."
                    },
                    "relatedTo": {
                        "ob_id": 8453,
                        "uuid": "bb890e4dd33645689c6fc769d9c1dc8f",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from AVHRR series at NOAA polar orbiting satellites for the NOAA Polar Orbiting Satellite Series Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: AVHRR series; PLATFORMS: NOAA polar orbiting satellites; "
                    }
                }
            ]
        },
        {
            "ob_id": 8465,
            "uuid": "72a8f18c43094de98711d1a399d51c8c",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from SHAC2000 E-Synthetic Aperture Radar at DLR Aircraft 2 (SHAC ESAR) for the SHAC Barton Bendish Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 E-Synthetic Aperture Radar; PLATFORMS: DLR Aircraft 2 (SHAC ESAR); ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8464,
                    "uuid": "6e50a2a20f6c4dd5804ec5602d83cf7a",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: DLR Aircraft 2 (SHAC ESAR)",
                    "abstract": "Mobile Platform Operation related to the: DLR Aircraft 2 (SHAC ESAR)"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2608,
                    "platform": {
                        "ob_id": 8462,
                        "uuid": "da07310c9d8d4382b2025c874ae7a89b",
                        "short_code": "plat",
                        "title": "DLR Aircraft 2 (SHAC ESAR)",
                        "abstract": "Platform.abstract: DETAILS NEEDED"
                    },
                    "instrument": {
                        "ob_id": 8463,
                        "uuid": "e55b2ba820cc4d30ba59d6bbe6ead70e",
                        "short_code": "instr",
                        "title": "SHAC2000 E-Synthetic Aperture Radar",
                        "abstract": "The SHAC2000 E-SAR is a multi-frequency Synthetic Aperture Radar (SAR) instrument. The special features of the E-SAR instrument are its very high resolution, flexible operating bands and polarisation, characteristics that allow high rates of data output and, by changing operating bands in flight, multi-band imaging. Multiple, successive flights were also flown enabling the extension of the polarimetric content at X- or C-bands."
                    },
                    "relatedTo": {
                        "ob_id": 8465,
                        "uuid": "72a8f18c43094de98711d1a399d51c8c",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from SHAC2000 E-Synthetic Aperture Radar at DLR Aircraft 2 (SHAC ESAR) for the SHAC Barton Bendish Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 E-Synthetic Aperture Radar; PLATFORMS: DLR Aircraft 2 (SHAC ESAR); "
                    }
                }
            ]
        },
        {
            "ob_id": 8469,
            "uuid": "de0c39e049034f39925a51fc40bdf324",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from SHAC2000 E-Synthetic Aperture Radar at DLR Aircraft 2 (SHAC ESAR) for the SHAC Boxworth Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 E-Synthetic Aperture Radar; PLATFORMS: DLR Aircraft 2 (SHAC ESAR); ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8464,
                    "uuid": "6e50a2a20f6c4dd5804ec5602d83cf7a",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: DLR Aircraft 2 (SHAC ESAR)",
                    "abstract": "Mobile Platform Operation related to the: DLR Aircraft 2 (SHAC ESAR)"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2609,
                    "platform": {
                        "ob_id": 8462,
                        "uuid": "da07310c9d8d4382b2025c874ae7a89b",
                        "short_code": "plat",
                        "title": "DLR Aircraft 2 (SHAC ESAR)",
                        "abstract": "Platform.abstract: DETAILS NEEDED"
                    },
                    "instrument": {
                        "ob_id": 8463,
                        "uuid": "e55b2ba820cc4d30ba59d6bbe6ead70e",
                        "short_code": "instr",
                        "title": "SHAC2000 E-Synthetic Aperture Radar",
                        "abstract": "The SHAC2000 E-SAR is a multi-frequency Synthetic Aperture Radar (SAR) instrument. The special features of the E-SAR instrument are its very high resolution, flexible operating bands and polarisation, characteristics that allow high rates of data output and, by changing operating bands in flight, multi-band imaging. Multiple, successive flights were also flown enabling the extension of the polarimetric content at X- or C-bands."
                    },
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                        "short_code": "acq",
                        "title": "Acquisition Process for: SHAC2000 Hyperspectral Mapper onboard DLR Aircraft 1 (SHAC Hymap) for SHAC Barton Bendish",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 Hyperspectral Mapper; PLATFORMS: DLR Aircraft 1 (SHAC Hymap); "
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        {
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            "short_code": "acq",
            "title": "Acquisition Process for: SHAC2000 Hyperspectral Mapper onboard DLR Aircraft 1 (SHAC Hymap) for SHAC Vryny",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 Hyperspectral Mapper; PLATFORMS: DLR Aircraft 1 (SHAC Hymap); ",
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            "short_code": "acq",
            "title": "Acquisition Process for: Data from SHAC2000 Hyperspectral Mapper at DLR Aircraft 1 (SHAC Hymap) for the SHAC Anglesey Campaign",
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            "mobilePlatformOperation": [
                {
                    "ob_id": 8057,
                    "uuid": "07dd9a71ab244b268c5d98f01d1d8a11",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: The Geoinformation Group (TGG) Survey Aircraft",
                    "abstract": "Mobile Platform Operation related to the: The Geoinformation Group (TGG) Survey Aircraft"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2632,
                    "platform": {
                        "ob_id": 8055,
                        "uuid": "9b8062d6c2914fe3904c0e9f21b299b1",
                        "short_code": "plat",
                        "title": "The Geoinformation Group (TGG) Survey Aircraft",
                        "abstract": "LiDAR-equipped survey aircraft owned by The GeoInformation Group were flown over the main urban conurbations of England and Scotland to provide LiDAR data for the Cities Revealed project."
                    },
                    "instrument": {
                        "ob_id": 8056,
                        "uuid": "72bbdd2fed4044de8371177cec47d9de",
                        "short_code": "instr",
                        "title": "UNDEFINED instrument associated with platform: The Geoinformation Group (TGG) Survey Aircraft",
                        "abstract": "This instrument is associated with the platform: The Geoinformation Group (TGG) Survey Aircraft"
                    },
                    "relatedTo": {
                        "ob_id": 8555,
                        "uuid": "943bdfaa17214cc1b0818378f98871a6",
                        "short_code": "acq",
                        "title": "Acquisition Process for: UK building classes",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: The Geoinformation Group (TGG) Survey Aircraft; PLATFORMS: The Geoinformation Group (TGG) Survey Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 8559,
            "uuid": "d8b246f1e88c4de4a07f9f26b7185477",
            "short_code": "acq",
            "title": "Acquisition Process for: UK building blocks",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: The Geoinformation Group (TGG) Survey Aircraft; PLATFORMS: The Geoinformation Group (TGG) Survey Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 8057,
                    "uuid": "07dd9a71ab244b268c5d98f01d1d8a11",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: The Geoinformation Group (TGG) Survey Aircraft",
                    "abstract": "Mobile Platform Operation related to the: The Geoinformation Group (TGG) Survey Aircraft"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2633,
                    "platform": {
                        "ob_id": 8055,
                        "uuid": "9b8062d6c2914fe3904c0e9f21b299b1",
                        "short_code": "plat",
                        "title": "The Geoinformation Group (TGG) Survey Aircraft",
                        "abstract": "LiDAR-equipped survey aircraft owned by The GeoInformation Group were flown over the main urban conurbations of England and Scotland to provide LiDAR data for the Cities Revealed project."
                    },
                    "instrument": {
                        "ob_id": 8056,
                        "uuid": "72bbdd2fed4044de8371177cec47d9de",
                        "short_code": "instr",
                        "title": "UNDEFINED instrument associated with platform: The Geoinformation Group (TGG) Survey Aircraft",
                        "abstract": "This instrument is associated with the platform: The Geoinformation Group (TGG) Survey Aircraft"
                    },
                    "relatedTo": {
                        "ob_id": 8559,
                        "uuid": "d8b246f1e88c4de4a07f9f26b7185477",
                        "short_code": "acq",
                        "title": "Acquisition Process for: UK building blocks",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: UNDEFINED instrument associated with platform: The Geoinformation Group (TGG) Survey Aircraft; PLATFORMS: The Geoinformation Group (TGG) Survey Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 8565,
            "uuid": "b7059644c4484dcd9fcb5a7f0a233458",
            "short_code": "acq",
            "title": "Acquisition Process for: Kinematic GPS (KGPS) data for UK roads",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Leica Geosystems System 500 and MC1000 units, Javad Eurocard receiver system, Leica choke-ring antenna; ",
            "imageDetails": [],
            "mobilePlatformOperation": [],
            "independentInstrument": [
                8562,
                8563,
                8564
            ],
            "instrumentplatformpair_set": []
        },
        {
            "ob_id": 8570,
            "uuid": "156e353d034846a58f4b92e778960422",
            "short_code": "acq",
            "title": "IASI (Infrared Atmospheric Sounding Interferometer) Instrument on board the Eumetsat EPS MetOp-A satellite.",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: IASI; 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": 2634,
                    "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": 8300,
                        "uuid": "57fc4dbabdf0434b9584836acac24ffe",
                        "short_code": "instr",
                        "title": "IASI",
                        "abstract": "Data from the IASI instruments on board the Eumetsat EPS MetOp satellite series. The Infrared Atmospheric Sounding Interferometer (IASI) is designed to measure the infrared spectrum emitted by the earth. IASI provides infrared soundings of the temperature profiles in the troposphere and lower stratosphere, moisture profiles in the troposphere, as well as some of the chemical components playing a key role in the climate monitoring, global change and atmospheric chemistry."
                    },
                    "relatedTo": {
                        "ob_id": 8570,
                        "uuid": "156e353d034846a58f4b92e778960422",
                        "short_code": "acq",
                        "title": "IASI (Infrared Atmospheric Sounding Interferometer) Instrument on board the Eumetsat EPS MetOp-A satellite.",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: IASI; PLATFORMS: Metop-A; "
                    }
                }
            ]
        },
        {
            "ob_id": 8575,
            "uuid": "a460b20f7ee54ee9b3030a6a22f29247",
            "short_code": "acq",
            "title": "Acquisition Process for: IASI Level 2 Data Products",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: IASI; 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": 2635,
                    "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": 8300,
                        "uuid": "57fc4dbabdf0434b9584836acac24ffe",
                        "short_code": "instr",
                        "title": "IASI",
                        "abstract": "Data from the IASI instruments on board the Eumetsat EPS MetOp satellite series. The Infrared Atmospheric Sounding Interferometer (IASI) is designed to measure the infrared spectrum emitted by the earth. IASI provides infrared soundings of the temperature profiles in the troposphere and lower stratosphere, moisture profiles in the troposphere, as well as some of the chemical components playing a key role in the climate monitoring, global change and atmospheric chemistry."
                    },
                    "relatedTo": {
                        "ob_id": 8575,
                        "uuid": "a460b20f7ee54ee9b3030a6a22f29247",
                        "short_code": "acq",
                        "title": "Acquisition Process for: IASI Level 2 Data Products",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: IASI; PLATFORMS: Metop-A; "
                    }
                }
            ]
        },
        {
            "ob_id": 8582,
            "uuid": "03a1ec76a906439ebdaa13e2e16901fa",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from Thematic Mapper (LS5) at Landsat5 for the Landsat Campaign",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Thematic Mapper (LS5); PLATFORMS: Landsat5; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
                    "ob_id": 7873,
                    "uuid": "1a6364279c8e4112846bfbd902248814",
                    "short_code": "mpop",
                    "title": "Mobile Platform Operation for: Landsat5",
                    "abstract": "Mobile Platform Operation related to the: Landsat5"
                }
            ],
            "independentInstrument": [],
            "instrumentplatformpair_set": [
                {
                    "ob_id": 2636,
                    "platform": {
                        "ob_id": 7871,
                        "uuid": "8f174632a60c4b11ac09cdce73943ff9",
                        "short_code": "plat",
                        "title": "Landsat5",
                        "abstract": "Landsat5 is a polar orbiting platform onboard which is mounted a Thematic Mapper (TM) and Multispectral Scanner (MSS) Instruments.\r\n\r\nLaunch date\t3/1/1984\r\nStatus / projected mission lifetime\tproject 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 (Landsat 5, descending node)\r\nSwath width\t183 km"
                    },
                    "instrument": {
                        "ob_id": 8581,
                        "uuid": "b78aa577f5a046889b3030ba63bd66f9",
                        "short_code": "instr",
                        "title": "Thematic Mapper (LS5)",
                        "abstract": "The Landsat5 Thematic Mapper is a a nadir-viewing, seven-band multi-spectral scanning radiometer instrument, almost identical to the LS4 TM. It was launched in 1984 and was in operation until at least April 2003. The Landsat TM sensor is capable of providing low to medium-resolution imaging information of the Earth's surface. The TM data are scanned simultaneously in seven spectral bands. Band 6 scans thermal (heat) infrared radiation. Spectral and spatial characteristics of these bands are shown below:\r\n\r\nBand no. 1\r\nSpectral range: .450 to .520 micrometres    Ground resolution: 30 m\r\nBand no. 2\r\nSpectral range:  .520 to .600 micrometres    Ground resolution: 30 m\r\nBand no. 3\r\nSpectral range:  .630 to .690  micrometres   Ground resolution: 30 m\r\nBand no. 4   \r\nSpectral range: .775 to .900  micrometres   Ground resolution: 30 m\r\nBand no. 5\r\nSpectral range: 1.550 to 1.750  micrometres Ground resolution: 30 m \r\nBand no. 6 \r\nSpectral range: 10.40 to 12.50  micrometres  Ground resolution: 120 m\r\nBand no. 7\r\nSpectral range:  2.080 to 2.350  micrometres  Ground resolution: 30 m"
                    },
                    "relatedTo": {
                        "ob_id": 8582,
                        "uuid": "03a1ec76a906439ebdaa13e2e16901fa",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from Thematic Mapper (LS5) at Landsat5 for the Landsat Campaign",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Thematic Mapper (LS5); PLATFORMS: Landsat5; "
                    }
                }
            ]
        },
        {
            "ob_id": 8597,
            "uuid": "d5101de07f484c58ad6486bc3600de4d",
            "short_code": "acq",
            "title": "Acquisition Process for: Atmospheric Retrievals from MIPAS/Envisat at Oxford v1.02-1.10",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Envisat - MIPAS (Michelson Interferometer for Passive Atmospheric Sounding (MIPAS) Instrument; 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": 2637,
                    "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": 8541,
                        "uuid": "0acdf61fc0444329869ce51541494552",
                        "short_code": "instr",
                        "title": "Envisat - MIPAS (Michelson Interferometer for Passive Atmospheric Sounding (MIPAS) Instrument",
                        "abstract": "The Michelson Interferometer for Passive Atmospheric Sounding (MIPAS) is one of the ten instruments onboard the Envisat satellite launched from Kourou (French Guyana) on the 28th February 2002 and operated by the European Space Agency (ESA). It operates as a Fourier transform spectrometer for the measurement of high-resolution gaseous emission spectra at the Earth's limb. It operates in the near- to mid-infrared, where many of the main atmospheric trace gases have important emission features. Its main objectives are to provide simultaneous and global measurements of the middle atmosphere dynamics, radiation budget and chemical composition (O3, H2O, CH4, N2O, HNO3, NO2), and to monitor stratospheric ozone and CFCs."
                    },
                    "relatedTo": {
                        "ob_id": 8597,
                        "uuid": "d5101de07f484c58ad6486bc3600de4d",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Atmospheric Retrievals from MIPAS/Envisat at Oxford v1.02-1.10",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: Envisat - MIPAS (Michelson Interferometer for Passive Atmospheric Sounding (MIPAS) Instrument; PLATFORMS: Envisat; "
                    }
                }
            ]
        },
        {
            "ob_id": 8609,
            "uuid": "ebbbe44b4a684749b5d6967a9539e0f7",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB05/16 over the Birmingham Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2638,
                    "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": 8609,
                        "uuid": "ebbbe44b4a684749b5d6967a9539e0f7",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB05/16 over the Birmingham Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8613,
            "uuid": "0625d6e94f694a2d8d6ec67b4aee2cc6",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB05/15 over the Fingringhoe Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2639,
                    "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": 8613,
                        "uuid": "0625d6e94f694a2d8d6ec67b4aee2cc6",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB05/15 over the Fingringhoe Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8617,
            "uuid": "c6ef83dcf41340b093bfff5b5bc9ce9b",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the CASI-2 Instrument on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2004/21 over the Chilbolton Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2640,
                    "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": 8617,
                        "uuid": "c6ef83dcf41340b093bfff5b5bc9ce9b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the CASI-2 Instrument on-board the Dornier Do228-101 D-CALM Aircraft during Flight GB2004/21 over the Chilbolton Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8622,
            "uuid": "0e6e225b2d214b9da8c9bd5a81738f65",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Optech LIDAR Instrument on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/09 over the Idrija and Ravne Faults, Slovenia",
            "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": 2641,
                    "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": 8622,
                        "uuid": "0e6e225b2d214b9da8c9bd5a81738f65",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Optech LIDAR Instrument on-board the Dornier Do228-101 D-CALM Aircraft during Flight MC04/09 over the Idrija and Ravne Faults, Slovenia",
                        "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": 8627,
            "uuid": "f387496fe28747698a0080469c35ce8b",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the ATM AZ-16 Instrument on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/28 over the Bath Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); 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": 2642,
                    "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": 8627,
                        "uuid": "f387496fe28747698a0080469c35ce8b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the ATM AZ-16 Instrument on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/28 over the Bath Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8631,
            "uuid": "f7a78bdb036845468c7bacd7d9e9a84c",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the ATM AZ-16 Instrument on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/20 for the Glass Sat Cal Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); 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": 2643,
                    "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": 8631,
                        "uuid": "f7a78bdb036845468c7bacd7d9e9a84c",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the ATM AZ-16 Instrument on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/20 for the Glass Sat Cal Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16); PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8635,
            "uuid": "069619d546a744cb8c1a8599af1ae21b",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Test Flight 04/999 over the Monks Wood Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2644,
                    "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": 8635,
                        "uuid": "069619d546a744cb8c1a8599af1ae21b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Test Flight 04/999 over the Monks Wood Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8639,
            "uuid": "a23876735dc0498b953522c6fef236c3",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/02 over Arctic Sea Ice",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2645,
                    "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": 8639,
                        "uuid": "a23876735dc0498b953522c6fef236c3",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/02 over Arctic Sea Ice",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8643,
            "uuid": "ea3b62fa23e849868881f99ce3d5eb2f",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/07 over the Reading 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); 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": 2646,
                    "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": 8643,
                        "uuid": "ea3b62fa23e849868881f99ce3d5eb2f",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/07 over the Reading 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); PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                },
                {
                    "ob_id": 2647,
                    "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": 8643,
                        "uuid": "ea3b62fa23e849868881f99ce3d5eb2f",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera and ATM AZ-16 Instruments on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/07 over the Reading 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); PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8647,
            "uuid": "6bcb6a5ed11540b68cc6f6908299f15a",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/22 over the Sound of Eriskay Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2648,
                    "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": 8647,
                        "uuid": "6bcb6a5ed11540b68cc6f6908299f15a",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/22 over the Sound of Eriskay Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8651,
            "uuid": "3cff84631b2a4986981f4bafdca277cf",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Calibration Flight 03/cal over the Monks Wood Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2649,
                    "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": 8651,
                        "uuid": "3cff84631b2a4986981f4bafdca277cf",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Calibration Flight 03/cal over the Monks Wood Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8655,
            "uuid": "bbb7c7b8b8154f1c8af5cdd3ac3850f4",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/xx over the Sawtry Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2650,
                    "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": 8655,
                        "uuid": "bbb7c7b8b8154f1c8af5cdd3ac3850f4",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 03/xx over the Sawtry Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8659,
            "uuid": "9ba6e26327ab4dff827372ea42ebf18c",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/04 over the Plymouth Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2651,
                    "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": 8659,
                        "uuid": "9ba6e26327ab4dff827372ea42ebf18c",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/04 over the Plymouth Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8663,
            "uuid": "17c470079ad449149fdc870095a48785",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/20 over the River Frome",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2652,
                    "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": 8663,
                        "uuid": "17c470079ad449149fdc870095a48785",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/20 over the River Frome",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8667,
            "uuid": "b9db36c7921a4347a54efc21ccc5fb15",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/35 over the Newport Bay Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2653,
                    "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": 8667,
                        "uuid": "b9db36c7921a4347a54efc21ccc5fb15",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/35 over the Newport Bay Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8671,
            "uuid": "8d91ca6a312c4bd0b6972b9adff58b7b",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/test over the Monks Wood Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2654,
                    "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": 8671,
                        "uuid": "8d91ca6a312c4bd0b6972b9adff58b7b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 02/test over the Monks Wood Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8675,
            "uuid": "7f1072d1630e4d01bae23c631ccabc3e",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 01/40 over the Black Ven Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2655,
                    "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": 8675,
                        "uuid": "7f1072d1630e4d01bae23c631ccabc3e",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 01/40 over the Black Ven Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8679,
            "uuid": "7f639cd8e4b9432c8150539838ed9e5a",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 01/41 for an Unnamed Project",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2656,
                    "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": 8679,
                        "uuid": "7f639cd8e4b9432c8150539838ed9e5a",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 01/41 for an Unnamed Project",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8683,
            "uuid": "5dd2001d0af04256a403bdaeca960755",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 01/42 over the Millingerwaard Area, Netherlands",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2657,
                    "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": 8683,
                        "uuid": "5dd2001d0af04256a403bdaeca960755",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 01/42 over the Millingerwaard Area, Netherlands",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF Compact Airbone Spectrographic Imager 2 (CASI-2); PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8687,
            "uuid": "0371d5b7f1b44e8b863ef31692dc5ab6",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 01/test over the Monks Wood Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2658,
                    "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": 8687,
                        "uuid": "0371d5b7f1b44e8b863ef31692dc5ab6",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Dornier Do228-101 D-CALM Aircraft during Flight 01/test over the Monks Wood Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Dornier Do228-101 D-CALM; "
                    }
                }
            ]
        },
        {
            "ob_id": 8693,
            "uuid": "b0d466a27d0b437188a65535abec1e63",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/01 over the Morbihan Area, France",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2659,
                    "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": 8693,
                        "uuid": "b0d466a27d0b437188a65535abec1e63",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/01 over the Morbihan Area, France",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 8697,
            "uuid": "ab30da7fef11468aa74ea450de9e02c7",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/20 over the Bedfordshire and Midlands Areas",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2660,
                    "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": 8697,
                        "uuid": "ab30da7fef11468aa74ea450de9e02c7",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/20 over the Bedfordshire and Midlands Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 8702,
            "uuid": "f230c01266d349f2a7516e106bf89334",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/22 over the New Forest Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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": 2661,
                    "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": 8702,
                        "uuid": "f230c01266d349f2a7516e106bf89334",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/22 over the New Forest Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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": 2662,
                    "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": 8702,
                        "uuid": "f230c01266d349f2a7516e106bf89334",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/22 over the New Forest Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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": 2663,
                    "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": 8702,
                        "uuid": "f230c01266d349f2a7516e106bf89334",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/22 over the New Forest Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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": 8706,
            "uuid": "7f545472753c46fa82176380796817eb",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/25 over the Isle of Islay",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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": 2664,
                    "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": 8706,
                        "uuid": "7f545472753c46fa82176380796817eb",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/25 over the Isle of Islay",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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": 2665,
                    "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": 8706,
                        "uuid": "7f545472753c46fa82176380796817eb",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/25 over the Isle of Islay",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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": 2666,
                    "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": 8706,
                        "uuid": "7f545472753c46fa82176380796817eb",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/25 over the Isle of Islay",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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": 8710,
            "uuid": "2a975513c67b4630b503c3556890f5f4",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/28 over the River Nith",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2667,
                    "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": 8710,
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                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/28 over the River Nith",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
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                }
            ]
        },
        {
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            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/test over the Monks Wood Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ",
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                {
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                    "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": [
                {
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                        "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": {
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                        "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."
                    },
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                        "uuid": "653ed747a96b4dc0932d4eb6ae1dda0b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 00/test over the Monks Wood Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
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        },
        {
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            "uuid": "3ef7dd8a97ec4136af68808d81a9fd58",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 97/18 over the Auchencarroch, Tarbolton Ayrshire and Greengairs Areas",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": [],
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                {
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                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
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                    },
                    "instrument": {
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                        "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."
                    },
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                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 97/18 over the Auchencarroch, Tarbolton Ayrshire and Greengairs Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
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        },
        {
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            "uuid": "9a8abcc79c58415daf0a00697269a35d",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 99/01 over the Alice Holt Area, Griffin Forest",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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; ",
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                    "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"
                }
            ],
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                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
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                    },
                    "instrument": {
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                        "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."
                    },
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                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 99/01 over the Alice Holt Area, Griffin Forest",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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; "
                    }
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                {
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                    "platform": {
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                        "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": {
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                        "short_code": "instr",
                        "title": "ARSF Compact Airbone Spectrographic Imager 1 (CASI-1)",
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                    },
                    "relatedTo": {
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                        "uuid": "9a8abcc79c58415daf0a00697269a35d",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 99/01 over the Alice Holt Area, Griffin Forest",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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; "
                    }
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                {
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                    "platform": {
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                        "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": {
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                        "short_code": "instr",
                        "title": "ARSF Airborne Thematic Mapper (ATM) Azimuth systems 16 (AZ-16)",
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                    },
                    "relatedTo": {
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                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 99/01 over the Alice Holt Area, Griffin Forest",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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; "
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        },
        {
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            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 99/08 over the Grimsby, Immingham and Hessle Areas",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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; ",
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            "mobilePlatformOperation": [
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                    "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": [],
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                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
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                    },
                    "instrument": {
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                        "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."
                    },
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                        "uuid": "920ab77c4af248db96ab35ae8e45d8da",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 99/08 over the Grimsby, Immingham and Hessle Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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; "
                    }
                },
                {
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                    "platform": {
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                        "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": {
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                        "uuid": "0207b70a7b5543de832f5a0d49320cbe",
                        "short_code": "instr",
                        "title": "ARSF Compact Airbone Spectrographic Imager 1 (CASI-1)",
                        "abstract": "NERC ARSF Compact Airborne Spectrographic Imager 1"
                    },
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                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 99/08 over the Grimsby, Immingham and Hessle Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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; "
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                {
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                    "platform": {
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                        "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": {
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                        "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"
                    },
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                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera, CASI and ATM AZ-16 Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 99/08 over the Grimsby, Immingham and Hessle Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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; "
                    }
                }
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        },
        {
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            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 98/06 over the Conington Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
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                    "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": [
                {
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                    "platform": {
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                        "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": {
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                        "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": {
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                        "uuid": "f44aa2b292c0457f8019a3908c372abc",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 98/06 over the Conington Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
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            "uuid": "c69b36f00b6c46aaaf8af5b935c781e1",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 98/xx over the North West Norfolk Area",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
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                    "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": [
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                    "platform": {
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                        "uuid": "af74710a0e4b400bafdd3669462728a2",
                        "short_code": "plat",
                        "title": "Piper PA31 Navajo Chieftain G-NERC Aircraft",
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                    },
                    "instrument": {
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                        "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."
                    },
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                        "ob_id": 8734,
                        "uuid": "c69b36f00b6c46aaaf8af5b935c781e1",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 98/xx over the North West Norfolk Area",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
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            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 94/09 over the Glensaugh, Sourhope (North), Sourhope (South), Drayton, Wytham, Rothamsted, Cairngorms, Snowdonia, Porton, Alice Holt, North Wyke and Moor House Areas",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
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                    "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": [
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                        "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": {
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                        "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": {
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                        "uuid": "d67b25a67ffc423186aed8946d860802",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 94/09 over the Glensaugh, Sourhope (North), Sourhope (South), Drayton, Wytham, Rothamsted, Cairngorms, Snowdonia, Porton, Alice Holt, North Wyke and Moor House Areas",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
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            "uuid": "652af580aff9443bad648b5e40d777e2",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 95/35 over the Ecomont Alps Area, Italy and Austria",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; ",
            "imageDetails": [],
            "mobilePlatformOperation": [
                {
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                    "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": [
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                        "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": {
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                        "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": 8742,
                        "uuid": "652af580aff9443bad648b5e40d777e2",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 95/35 over the Ecomont Alps Area, Italy and Austria",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 8746,
            "uuid": "a25b21ad66894f0b966a6dbd1d6ad263",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 97/21 over the Tweed Estuary and Humber Estuary, in support of the Land-Ocean Interaction Study (LOIS) and the Rivers, Atmosphere and Coasts Study (RACS)",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2680,
                    "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": 8746,
                        "uuid": "a25b21ad66894f0b966a6dbd1d6ad263",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 97/21 over the Tweed Estuary and Humber Estuary, in support of the Land-Ocean Interaction Study (LOIS) and the Rivers, Atmosphere and Coasts Study (RACS)",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 8750,
            "uuid": "b39e24a409414fc09b90d7f27c9e3c80",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 97/test over the Storebaelt Bridge Area, Denmark",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2681,
                    "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": 8750,
                        "uuid": "b39e24a409414fc09b90d7f27c9e3c80",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 97/test over the Storebaelt Bridge Area, Denmark",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 8755,
            "uuid": "fda5653dad4e4ef7a49c77441021475b",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 95/16 over the Rodalquilar Area, Spain",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, 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": 2682,
                    "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": 8755,
                        "uuid": "fda5653dad4e4ef7a49c77441021475b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 95/16 over the Rodalquilar Area, Spain",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                },
                {
                    "ob_id": 2683,
                    "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": 8755,
                        "uuid": "fda5653dad4e4ef7a49c77441021475b",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera and ATM Instruments on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 95/16 over the Rodalquilar Area, Spain",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera, ARSF Airborne Thematic Mapper (ATM) Daedalus-1268; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        },
        {
            "ob_id": 8759,
            "uuid": "d1f1d37cb0254505b50f5e31c5ef9dd3",
            "short_code": "acq",
            "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 95/20 over the Tweed Estuary",
            "abstract": "This acquisition is comprised of the following: INSTRUMENTS: 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": 2684,
                    "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": 8759,
                        "uuid": "d1f1d37cb0254505b50f5e31c5ef9dd3",
                        "short_code": "acq",
                        "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 95/20 over the Tweed Estuary",
                        "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
                    }
                }
            ]
        }
    ]
}