Instrument Platform Pair List

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    "count": 14115,
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    "results": [
        {
            "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": 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": 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": 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": 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": 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."
            },
            "relatedTo": {
                "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); "
            }
        },
        {
            "ob_id": 2610,
            "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": 8473,
                "uuid": "18db03201a904384afeee9e32b952cb5",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 E-Synthetic Aperture Radar at DLR Aircraft 2 (SHAC ESAR) for the SHAC Glen Affric Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 E-Synthetic Aperture Radar; PLATFORMS: DLR Aircraft 2 (SHAC ESAR); "
            }
        },
        {
            "ob_id": 2611,
            "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": 8477,
                "uuid": "ff659fdae5684f61bd27db55ef1df8ec",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 E-Synthetic Aperture Radar at DLR Aircraft 2 (SHAC ESAR) for the SHAC Longendale Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 E-Synthetic Aperture Radar; PLATFORMS: DLR Aircraft 2 (SHAC ESAR); "
            }
        },
        {
            "ob_id": 2612,
            "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": 8481,
                "uuid": "772e5f89b05946eabee8911094cc97fc",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 E-Synthetic Aperture Radar at DLR Aircraft 2 (SHAC ESAR) for the SHAC Monkswood Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 E-Synthetic Aperture Radar; PLATFORMS: DLR Aircraft 2 (SHAC ESAR); "
            }
        },
        {
            "ob_id": 2613,
            "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": 8485,
                "uuid": "4f7ddc146f2341ee8b4f116f0312f21d",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 E-Synthetic Aperture Radar at DLR Aircraft 2 (SHAC ESAR) for the SHAC Tay Estuary Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 E-Synthetic Aperture Radar; PLATFORMS: DLR Aircraft 2 (SHAC ESAR); "
            }
        },
        {
            "ob_id": 2614,
            "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": 8489,
                "uuid": "18a83334de464b2ab993fc409a44c5cb",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 E-Synthetic Aperture Radar at DLR Aircraft 2 (SHAC ESAR) for the SHAC Thetford Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 E-Synthetic Aperture Radar; PLATFORMS: DLR Aircraft 2 (SHAC ESAR); "
            }
        },
        {
            "ob_id": 2615,
            "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": 8493,
                "uuid": "ec799c54d0554b32b21142d857b19e13",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 E-Synthetic Aperture Radar at DLR Aircraft 2 (SHAC ESAR) for the SHAC Vryny Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 E-Synthetic Aperture Radar; PLATFORMS: DLR Aircraft 2 (SHAC ESAR); "
            }
        },
        {
            "ob_id": 2616,
            "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": 8497,
                "uuid": "b91a66bad7c7459187ce673dc79f83b3",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 E-Synthetic Aperture Radar at DLR Aircraft 2 (SHAC ESAR) for the SHAC West Harling Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 E-Synthetic Aperture Radar; PLATFORMS: DLR Aircraft 2 (SHAC ESAR); "
            }
        },
        {
            "ob_id": 2617,
            "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": 8501,
                "uuid": "df04dfa911ed403fb305b8c937d3fe2e",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 E-Synthetic Aperture Radar at DLR Aircraft 2 (SHAC ESAR) for the SHAC Wrangle Flats Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 E-Synthetic Aperture Radar; PLATFORMS: DLR Aircraft 2 (SHAC ESAR); "
            }
        },
        {
            "ob_id": 2618,
            "platform": {
                "ob_id": 8504,
                "uuid": "d31371f3716143fb957a55dbad558c64",
                "short_code": "plat",
                "title": "DLR Aircraft 1 (SHAC Hymap)",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "instrument": {
                "ob_id": 8505,
                "uuid": "1ff689f1398249d3aecc2157147681db",
                "short_code": "instr",
                "title": "SHAC2000 Hyperspectral Mapper",
                "abstract": "The Hyper-spectral Mapper operated by HyVista and built by Integrated Spectronics of Australia, differed from other sensors used in the UK by having 126 narrow, contiguous channels of data across the entire visible to shortwave infrared wavelength bands. Spectral coverage is continuous except for near the 1.4 um and 1.9 um bands. The instrument (see Fig.1) operates optimally at a spatial resolution of 5 m giving a 2.3 km swath width, which can be varied to a resolution of 3 m and a swath width of 1.3 m but at the expense of reduced signal to noise ratios at SWIR wavelengths."
            },
            "relatedTo": {
                "ob_id": 8507,
                "uuid": "e0676596c208466c9ebd552d3169d69d",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 Hyperspectral Mapper at DLR Aircraft 1 (SHAC Hymap) for the SHAC Monkswood Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 Hyperspectral Mapper; PLATFORMS: DLR Aircraft 1 (SHAC Hymap); "
            }
        },
        {
            "ob_id": 2619,
            "platform": {
                "ob_id": 8504,
                "uuid": "d31371f3716143fb957a55dbad558c64",
                "short_code": "plat",
                "title": "DLR Aircraft 1 (SHAC Hymap)",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "instrument": {
                "ob_id": 8505,
                "uuid": "1ff689f1398249d3aecc2157147681db",
                "short_code": "instr",
                "title": "SHAC2000 Hyperspectral Mapper",
                "abstract": "The Hyper-spectral Mapper operated by HyVista and built by Integrated Spectronics of Australia, differed from other sensors used in the UK by having 126 narrow, contiguous channels of data across the entire visible to shortwave infrared wavelength bands. Spectral coverage is continuous except for near the 1.4 um and 1.9 um bands. The instrument (see Fig.1) operates optimally at a spatial resolution of 5 m giving a 2.3 km swath width, which can be varied to a resolution of 3 m and a swath width of 1.3 m but at the expense of reduced signal to noise ratios at SWIR wavelengths."
            },
            "relatedTo": {
                "ob_id": 8510,
                "uuid": "bcc9486edceb4e02bcd503475b9b2906",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 Hyperspectral Mapper at DLR Aircraft 1 (SHAC Hymap) for the SHAC Thetford Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 Hyperspectral Mapper; PLATFORMS: DLR Aircraft 1 (SHAC Hymap); "
            }
        },
        {
            "ob_id": 2620,
            "platform": {
                "ob_id": 8504,
                "uuid": "d31371f3716143fb957a55dbad558c64",
                "short_code": "plat",
                "title": "DLR Aircraft 1 (SHAC Hymap)",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "instrument": {
                "ob_id": 8505,
                "uuid": "1ff689f1398249d3aecc2157147681db",
                "short_code": "instr",
                "title": "SHAC2000 Hyperspectral Mapper",
                "abstract": "The Hyper-spectral Mapper operated by HyVista and built by Integrated Spectronics of Australia, differed from other sensors used in the UK by having 126 narrow, contiguous channels of data across the entire visible to shortwave infrared wavelength bands. Spectral coverage is continuous except for near the 1.4 um and 1.9 um bands. The instrument (see Fig.1) operates optimally at a spatial resolution of 5 m giving a 2.3 km swath width, which can be varied to a resolution of 3 m and a swath width of 1.3 m but at the expense of reduced signal to noise ratios at SWIR wavelengths."
            },
            "relatedTo": {
                "ob_id": 8513,
                "uuid": "81eba790c5ba4c4cb981254de670f81c",
                "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); "
            }
        },
        {
            "ob_id": 2621,
            "platform": {
                "ob_id": 8504,
                "uuid": "d31371f3716143fb957a55dbad558c64",
                "short_code": "plat",
                "title": "DLR Aircraft 1 (SHAC Hymap)",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "instrument": {
                "ob_id": 8505,
                "uuid": "1ff689f1398249d3aecc2157147681db",
                "short_code": "instr",
                "title": "SHAC2000 Hyperspectral Mapper",
                "abstract": "The Hyper-spectral Mapper operated by HyVista and built by Integrated Spectronics of Australia, differed from other sensors used in the UK by having 126 narrow, contiguous channels of data across the entire visible to shortwave infrared wavelength bands. Spectral coverage is continuous except for near the 1.4 um and 1.9 um bands. The instrument (see Fig.1) operates optimally at a spatial resolution of 5 m giving a 2.3 km swath width, which can be varied to a resolution of 3 m and a swath width of 1.3 m but at the expense of reduced signal to noise ratios at SWIR wavelengths."
            },
            "relatedTo": {
                "ob_id": 8516,
                "uuid": "3af4d887de644b699fd6fd6f3b9f1653",
                "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); "
            }
        },
        {
            "ob_id": 2622,
            "platform": {
                "ob_id": 8504,
                "uuid": "d31371f3716143fb957a55dbad558c64",
                "short_code": "plat",
                "title": "DLR Aircraft 1 (SHAC Hymap)",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "instrument": {
                "ob_id": 8505,
                "uuid": "1ff689f1398249d3aecc2157147681db",
                "short_code": "instr",
                "title": "SHAC2000 Hyperspectral Mapper",
                "abstract": "The Hyper-spectral Mapper operated by HyVista and built by Integrated Spectronics of Australia, differed from other sensors used in the UK by having 126 narrow, contiguous channels of data across the entire visible to shortwave infrared wavelength bands. Spectral coverage is continuous except for near the 1.4 um and 1.9 um bands. The instrument (see Fig.1) operates optimally at a spatial resolution of 5 m giving a 2.3 km swath width, which can be varied to a resolution of 3 m and a swath width of 1.3 m but at the expense of reduced signal to noise ratios at SWIR wavelengths."
            },
            "relatedTo": {
                "ob_id": 8520,
                "uuid": "36369014b8ff4f52820adb3f65b07b0c",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 Hyperspectral Mapper at DLR Aircraft 1 (SHAC Hymap) for the SHAC Anglesey Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 Hyperspectral Mapper; PLATFORMS: DLR Aircraft 1 (SHAC Hymap); "
            }
        },
        {
            "ob_id": 2623,
            "platform": {
                "ob_id": 8504,
                "uuid": "d31371f3716143fb957a55dbad558c64",
                "short_code": "plat",
                "title": "DLR Aircraft 1 (SHAC Hymap)",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "instrument": {
                "ob_id": 8505,
                "uuid": "1ff689f1398249d3aecc2157147681db",
                "short_code": "instr",
                "title": "SHAC2000 Hyperspectral Mapper",
                "abstract": "The Hyper-spectral Mapper operated by HyVista and built by Integrated Spectronics of Australia, differed from other sensors used in the UK by having 126 narrow, contiguous channels of data across the entire visible to shortwave infrared wavelength bands. Spectral coverage is continuous except for near the 1.4 um and 1.9 um bands. The instrument (see Fig.1) operates optimally at a spatial resolution of 5 m giving a 2.3 km swath width, which can be varied to a resolution of 3 m and a swath width of 1.3 m but at the expense of reduced signal to noise ratios at SWIR wavelengths."
            },
            "relatedTo": {
                "ob_id": 8523,
                "uuid": "2f7e6480de31497da9efd3bf0f2cede9",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 Hyperspectral Mapper at DLR Aircraft 1 (SHAC Hymap) for the SHAC Longendale Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 Hyperspectral Mapper; PLATFORMS: DLR Aircraft 1 (SHAC Hymap); "
            }
        },
        {
            "ob_id": 2624,
            "platform": {
                "ob_id": 8504,
                "uuid": "d31371f3716143fb957a55dbad558c64",
                "short_code": "plat",
                "title": "DLR Aircraft 1 (SHAC Hymap)",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "instrument": {
                "ob_id": 8505,
                "uuid": "1ff689f1398249d3aecc2157147681db",
                "short_code": "instr",
                "title": "SHAC2000 Hyperspectral Mapper",
                "abstract": "The Hyper-spectral Mapper operated by HyVista and built by Integrated Spectronics of Australia, differed from other sensors used in the UK by having 126 narrow, contiguous channels of data across the entire visible to shortwave infrared wavelength bands. Spectral coverage is continuous except for near the 1.4 um and 1.9 um bands. The instrument (see Fig.1) operates optimally at a spatial resolution of 5 m giving a 2.3 km swath width, which can be varied to a resolution of 3 m and a swath width of 1.3 m but at the expense of reduced signal to noise ratios at SWIR wavelengths."
            },
            "relatedTo": {
                "ob_id": 8527,
                "uuid": "e777b48beb9f413da4bd643b98f0aee3",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 Hyperspectral Mapper at DLR Aircraft 1 (SHAC Hymap) for the SHAC Rosemaund Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 Hyperspectral Mapper; PLATFORMS: DLR Aircraft 1 (SHAC Hymap); "
            }
        },
        {
            "ob_id": 2625,
            "platform": {
                "ob_id": 8504,
                "uuid": "d31371f3716143fb957a55dbad558c64",
                "short_code": "plat",
                "title": "DLR Aircraft 1 (SHAC Hymap)",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "instrument": {
                "ob_id": 8505,
                "uuid": "1ff689f1398249d3aecc2157147681db",
                "short_code": "instr",
                "title": "SHAC2000 Hyperspectral Mapper",
                "abstract": "The Hyper-spectral Mapper operated by HyVista and built by Integrated Spectronics of Australia, differed from other sensors used in the UK by having 126 narrow, contiguous channels of data across the entire visible to shortwave infrared wavelength bands. Spectral coverage is continuous except for near the 1.4 um and 1.9 um bands. The instrument (see Fig.1) operates optimally at a spatial resolution of 5 m giving a 2.3 km swath width, which can be varied to a resolution of 3 m and a swath width of 1.3 m but at the expense of reduced signal to noise ratios at SWIR wavelengths."
            },
            "relatedTo": {
                "ob_id": 8531,
                "uuid": "9ea1c06be78e4b9393dacdc00811b4e4",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 Hyperspectral Mapper at DLR Aircraft 1 (SHAC Hymap) for the SHAC Titley Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 Hyperspectral Mapper; PLATFORMS: DLR Aircraft 1 (SHAC Hymap); "
            }
        },
        {
            "ob_id": 2626,
            "platform": {
                "ob_id": 8504,
                "uuid": "d31371f3716143fb957a55dbad558c64",
                "short_code": "plat",
                "title": "DLR Aircraft 1 (SHAC Hymap)",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "instrument": {
                "ob_id": 8505,
                "uuid": "1ff689f1398249d3aecc2157147681db",
                "short_code": "instr",
                "title": "SHAC2000 Hyperspectral Mapper",
                "abstract": "The Hyper-spectral Mapper operated by HyVista and built by Integrated Spectronics of Australia, differed from other sensors used in the UK by having 126 narrow, contiguous channels of data across the entire visible to shortwave infrared wavelength bands. Spectral coverage is continuous except for near the 1.4 um and 1.9 um bands. The instrument (see Fig.1) operates optimally at a spatial resolution of 5 m giving a 2.3 km swath width, which can be varied to a resolution of 3 m and a swath width of 1.3 m but at the expense of reduced signal to noise ratios at SWIR wavelengths."
            },
            "relatedTo": {
                "ob_id": 8535,
                "uuid": "921720f121c34216a8ef802553a94c91",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from SHAC2000 Hyperspectral Mapper at DLR Aircraft 1 (SHAC Hymap) for the SHAC New Forest Campaign",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: SHAC2000 Hyperspectral Mapper; PLATFORMS: DLR Aircraft 1 (SHAC Hymap); "
            }
        },
        {
            "ob_id": 2627,
            "platform": {
                "ob_id": 8539,
                "uuid": "b5127b97a85243b2ba26a8766573614b",
                "short_code": "plat",
                "title": "ESA ENVISAT Processing Ground Station",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "instrument": {
                "ob_id": 8540,
                "uuid": "823c2bdc449e41aa8fa6c60db1074983",
                "short_code": "instr",
                "title": "MIPAS Level 1b data processing",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
            "relatedTo": {
                "ob_id": 8542,
                "uuid": "38540b15ec714e46a2751696247d9256",
                "short_code": "acq",
                "title": "Acquisition Process for: ENVISAT MIPAS Level 1b consolidated, near-real time and reprocessed data (March 2002 - April 2012)",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: MIPAS Level 1b data processing, Envisat - MIPAS (Michelson Interferometer for Passive Atmospheric Sounding (MIPAS) Instrument; PLATFORMS: ESA ENVISAT Processing Ground Station; "
            }
        },
        {
            "ob_id": 2628,
            "platform": {
                "ob_id": 8539,
                "uuid": "b5127b97a85243b2ba26a8766573614b",
                "short_code": "plat",
                "title": "ESA ENVISAT Processing Ground Station",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "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": 8542,
                "uuid": "38540b15ec714e46a2751696247d9256",
                "short_code": "acq",
                "title": "Acquisition Process for: ENVISAT MIPAS Level 1b consolidated, near-real time and reprocessed data (March 2002 - April 2012)",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: MIPAS Level 1b data processing, Envisat - MIPAS (Michelson Interferometer for Passive Atmospheric Sounding (MIPAS) Instrument; PLATFORMS: ESA ENVISAT Processing Ground Station; "
            }
        },
        {
            "ob_id": 2629,
            "platform": {
                "ob_id": 8539,
                "uuid": "b5127b97a85243b2ba26a8766573614b",
                "short_code": "plat",
                "title": "ESA ENVISAT Processing Ground Station",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "instrument": {
                "ob_id": 8545,
                "uuid": "663980a1ea8f40dab48d39077caf43be",
                "short_code": "instr",
                "title": "MIPAS Level 2 data processing",
                "abstract": "Instrument.abstract: DETAILS NEEDED"
            },
            "relatedTo": {
                "ob_id": 8546,
                "uuid": "848a92ae94f64fc48bbba881bd918fb1",
                "short_code": "acq",
                "title": "Acquisition Process for: ENVISAT MIPAS Level 2 consolidated and reprocessed data (July 2002 - March 2004)",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: MIPAS Level 2 data processing, Envisat - MIPAS (Michelson Interferometer for Passive Atmospheric Sounding (MIPAS) Instrument; PLATFORMS: ESA ENVISAT Processing Ground Station; "
            }
        },
        {
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            "platform": {
                "ob_id": 8539,
                "uuid": "b5127b97a85243b2ba26a8766573614b",
                "short_code": "plat",
                "title": "ESA ENVISAT Processing Ground Station",
                "abstract": "Platform.abstract: DETAILS NEEDED"
            },
            "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": 8546,
                "uuid": "848a92ae94f64fc48bbba881bd918fb1",
                "short_code": "acq",
                "title": "Acquisition Process for: ENVISAT MIPAS Level 2 consolidated and reprocessed data (July 2002 - March 2004)",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: MIPAS Level 2 data processing, Envisat - MIPAS (Michelson Interferometer for Passive Atmospheric Sounding (MIPAS) Instrument; PLATFORMS: ESA ENVISAT Processing Ground Station; "
            }
        },
        {
            "ob_id": 2631,
            "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": 8551,
                "uuid": "c4d1324a7993448d9ba006a09972937e",
                "short_code": "acq",
                "title": "Acquisition Process for: UK building heights",
                "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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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": 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,
                "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; "
            }
        },
        {
            "ob_id": 2668,
            "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": 8714,
                "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; "
            }
        },
        {
            "ob_id": 2669,
            "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": 8718,
                "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; "
            }
        },
        {
            "ob_id": 2670,
            "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": 8722,
                "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; "
            }
        },
        {
            "ob_id": 2671,
            "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": 8722,
                "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; "
            }
        },
        {
            "ob_id": 2672,
            "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": 8722,
                "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; "
            }
        },
        {
            "ob_id": 2673,
            "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": 8726,
                "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; "
            }
        },
        {
            "ob_id": 2674,
            "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": 8726,
                "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; "
            }
        },
        {
            "ob_id": 2675,
            "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": 8726,
                "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; "
            }
        },
        {
            "ob_id": 2676,
            "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": 8730,
                "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; "
            }
        },
        {
            "ob_id": 2677,
            "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": 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; "
            }
        },
        {
            "ob_id": 2678,
            "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": 8738,
                "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; "
            }
        },
        {
            "ob_id": 2679,
            "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": 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": 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": 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": 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": 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; "
            }
        },
        {
            "ob_id": 2685,
            "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": 8763,
                "uuid": "400bc2fb32f9415f83386a1df2bce0d3",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 95/29 over the Rodaliquilar and Carboneras Areas, Spain",
                "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": 2686,
            "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": 8767,
                "uuid": "002ec9d1dac940778893c16e7f9b6677",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 95/30 over the Coto Donana Area, Spain",
                "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": 2687,
            "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": 8771,
                "uuid": "3bf28b05d905486090ab8f5435645a4b",
                "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 95/34 over the Lake Vrywny Area",
                "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": 2688,
            "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": 8771,
                "uuid": "3bf28b05d905486090ab8f5435645a4b",
                "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 95/34 over the Lake Vrywny Area",
                "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": 2689,
            "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": 8775,
                "uuid": "3ca23f322e7c4e4d95e896d9fda3ea35",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 93/05 over the Portugos Area, Spain",
                "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": 2690,
            "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": 8779,
                "uuid": "9968f4a879374a37b58e5fe4a8dda5dd",
                "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 96/02 over the Llanbrynmair Moor Area",
                "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": 2691,
            "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": 8779,
                "uuid": "9968f4a879374a37b58e5fe4a8dda5dd",
                "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 96/02 over the Llanbrynmair Moor Area",
                "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": 2692,
            "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": 8783,
                "uuid": "0a587af881bc41459585dd2fca27ebe5",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 96/23 over the Puerto Lumbreras, Embalse de Puentes and Las Palas Areas, Spain",
                "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": 2693,
            "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": 8787,
                "uuid": "fc7f346769684840890196822f9877d1",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 96/28 over the Las Palas and Puerto Lumbreras Areas, Spain",
                "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": 2694,
            "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": 8791,
                "uuid": "5af77230fd814912911832e6f48334da",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 96/29 over the Rambla Honda, Velez del Rubio, and Ramble de Nogalte Areas, Spain",
                "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": 2695,
            "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": 8795,
                "uuid": "8f538fdf734a40b6930d9154b50c0f27",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 96/30 over the Rambla Honda, Velez del Rubio, Rambla de Nogalte and Rambla del Chortal Areas, Spain",
                "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": 2696,
            "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": 8799,
                "uuid": "cb8a0fab685b44a2895dbdb606093725",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 96/32 over the Salisbury Plain Area",
                "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": 2697,
            "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": 8803,
                "uuid": "73990c4421fd4aa382c5ac1e030ffac6",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 96/33 over the Porton Down Area",
                "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": 2698,
            "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": 8807,
                "uuid": "5a4b0508bc164539b3627be8d1d19add",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 96/34 over the Lake Vrywny Area",
                "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": 2699,
            "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": 8811,
                "uuid": "bd9102ebe401450582023ccad1dc0b5d",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 96/36 over the Walsall and Wolverhampton 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": 2700,
            "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": 8815,
                "uuid": "29ef9a836d994969a9003756a3426f68",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 96/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; "
            }
        },
        {
            "ob_id": 2701,
            "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": 8819,
                "uuid": "de6df72082024fcfb5d9f75b69da1000",
                "short_code": "acq",
                "title": "Acquisition Process for: Data from the Photographic Camera on-board the Piper PA31 Navajo Chieftain G-NERC Aircraft during Flight 96/xx over the Llyn Brianne Area",
                "abstract": "This acquisition is comprised of the following: INSTRUMENTS: ARSF WILD-RC10 Analogue Photographic camera; PLATFORMS: Piper PA31 Navajo Chieftain G-NERC Aircraft; "
            }
        }
    ]
}