Instrument Platform Pair List
Get a list of InstrumentPlaformPair objects. InstrumentPlaformPairs are used within Acquisitions which
enable linking between Instruments, Platforms and Observations (though may be via CompositeProcesses).
GET /api/v3/ipps/?format=api&offset=10600
{ "count": 14115, "next": "https://api.catalogue.ceda.ac.uk/api/v3/ipps/?format=api&limit=100&offset=10700", "previous": "https://api.catalogue.ceda.ac.uk/api/v3/ipps/?format=api&limit=100&offset=10500", "results": [ { "ob_id": 11005, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24141, "uuid": "e7609d8e116d4f54b49eabf3331a2707", "short_code": "acq", "title": "INTACASA-RS EUFAR HYPERFOREST Flight, 2010-08-31: data acquisition details", "abstract": "INTACASA-RS EUFAR HYPERFOREST Flight, 2010-08-31 data acquisition details." } }, { "ob_id": 11006, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24141, "uuid": "e7609d8e116d4f54b49eabf3331a2707", "short_code": "acq", "title": "INTACASA-RS EUFAR HYPERFOREST Flight, 2010-08-31: data acquisition details", "abstract": "INTACASA-RS EUFAR HYPERFOREST Flight, 2010-08-31 data acquisition details." } }, { "ob_id": 11007, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24145, "uuid": "2b924fdc259b431d9ca0bea118b41d12", "short_code": "acq", "title": "INTACASA-RS EUFAR HYPERFOREST Flight, 2010-09-01: data acquisition details", "abstract": "INTACASA-RS EUFAR HYPERFOREST Flight, 2010-09-01 data acquisition details." } }, { "ob_id": 11008, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24145, "uuid": "2b924fdc259b431d9ca0bea118b41d12", "short_code": "acq", "title": "INTACASA-RS EUFAR HYPERFOREST Flight, 2010-09-01: data acquisition details", "abstract": "INTACASA-RS EUFAR HYPERFOREST Flight, 2010-09-01 data acquisition details." } }, { "ob_id": 11009, "platform": { "ob_id": 11911, "uuid": "8291c6659fb04c0ead2af01941a79c0e", "short_code": "plat", "title": "ATR42 - SAFIRE aircraft", "abstract": "ATR42-SAFIRE is a large tropospheric research aircraft operated by Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe ATR 42 is a twin-turboprop, short-haul regional airliner built in France and Italy by ATR. The name \"42\" comes from the aircraft's standard seating, which varies from 40 to 52. The ATR-42 320 was designed to have better performance especially in hot and high conditions. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20344, "uuid": "9229a752355a4684b4a6c3b1dbdbe160", "short_code": "instr", "title": "SAFIRE ATR42 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-ATR42 aircraft. Includes Inertial Reference/Navigation System, Non dew/frost point hygrometer, Incident flow vector probe, Dew/Frost-point hygrometer, Global Positioning System, Broad Band Radiometer (x2), Temperature sensor (in situ) and Inertial Reference/Navigation System. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24149, "uuid": "edacbcfc08424c50987bbf4c14fbf96f", "short_code": "acq", "title": "SAFIRE-ATR42 AS39 EUFAR I-WAKE2 Flight, 2010-08-26: data acquisition details", "abstract": "SAFIRE-ATR42 AS39 EUFAR I-WAKE2 Flight, 2010-08-26 data acquisition details." } }, { "ob_id": 11010, "platform": { "ob_id": 11911, "uuid": "8291c6659fb04c0ead2af01941a79c0e", "short_code": "plat", "title": "ATR42 - SAFIRE aircraft", "abstract": "ATR42-SAFIRE is a large tropospheric research aircraft operated by Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe ATR 42 is a twin-turboprop, short-haul regional airliner built in France and Italy by ATR. The name \"42\" comes from the aircraft's standard seating, which varies from 40 to 52. The ATR-42 320 was designed to have better performance especially in hot and high conditions. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20344, "uuid": "9229a752355a4684b4a6c3b1dbdbe160", "short_code": "instr", "title": "SAFIRE ATR42 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-ATR42 aircraft. Includes Inertial Reference/Navigation System, Non dew/frost point hygrometer, Incident flow vector probe, Dew/Frost-point hygrometer, Global Positioning System, Broad Band Radiometer (x2), Temperature sensor (in situ) and Inertial Reference/Navigation System. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24154, "uuid": "e950304c581c4b2e89a54ee0956e1ba0", "short_code": "acq", "title": "SAFIRE-ATR42 AS42 EUFAR I-WAKE2 Flight, 2010-08-30: data acquisition details", "abstract": "SAFIRE-ATR42 AS42 EUFAR I-WAKE2 Flight, 2010-08-30 data acquisition details." } }, { "ob_id": 11011, "platform": { "ob_id": 11911, "uuid": "8291c6659fb04c0ead2af01941a79c0e", "short_code": "plat", "title": "ATR42 - SAFIRE aircraft", "abstract": "ATR42-SAFIRE is a large tropospheric research aircraft operated by Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe ATR 42 is a twin-turboprop, short-haul regional airliner built in France and Italy by ATR. The name \"42\" comes from the aircraft's standard seating, which varies from 40 to 52. The ATR-42 320 was designed to have better performance especially in hot and high conditions. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20344, "uuid": "9229a752355a4684b4a6c3b1dbdbe160", "short_code": "instr", "title": "SAFIRE ATR42 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-ATR42 aircraft. Includes Inertial Reference/Navigation System, Non dew/frost point hygrometer, Incident flow vector probe, Dew/Frost-point hygrometer, Global Positioning System, Broad Band Radiometer (x2), Temperature sensor (in situ) and Inertial Reference/Navigation System. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24158, "uuid": "f16762dfb67545fda5a7fc65c9f9f610", "short_code": "acq", "title": "SAFIRE-ATR42 AS44 EUFAR I-WAKE2 Flight, 2010-09-02: data acquisition details", "abstract": "SAFIRE-ATR42 AS44 EUFAR I-WAKE2 Flight, 2010-09-02 data acquisition details." } }, { "ob_id": 11012, "platform": { "ob_id": 11911, "uuid": "8291c6659fb04c0ead2af01941a79c0e", "short_code": "plat", "title": "ATR42 - SAFIRE aircraft", "abstract": "ATR42-SAFIRE is a large tropospheric research aircraft operated by Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe ATR 42 is a twin-turboprop, short-haul regional airliner built in France and Italy by ATR. The name \"42\" comes from the aircraft's standard seating, which varies from 40 to 52. The ATR-42 320 was designed to have better performance especially in hot and high conditions. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20344, "uuid": "9229a752355a4684b4a6c3b1dbdbe160", "short_code": "instr", "title": "SAFIRE ATR42 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-ATR42 aircraft. Includes Inertial Reference/Navigation System, Non dew/frost point hygrometer, Incident flow vector probe, Dew/Frost-point hygrometer, Global Positioning System, Broad Band Radiometer (x2), Temperature sensor (in situ) and Inertial Reference/Navigation System. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24162, "uuid": "f66e920b02834c81b21d4827589ec0b0", "short_code": "acq", "title": "SAFIRE-ATR42 AS45 EUFAR I-WAKE2 Flight, 2010-09-02: data acquisition details", "abstract": "SAFIRE-ATR42 AS45 EUFAR I-WAKE2 Flight, 2010-09-02 data acquisition details." } }, { "ob_id": 11013, "platform": { "ob_id": 11911, "uuid": "8291c6659fb04c0ead2af01941a79c0e", "short_code": "plat", "title": "ATR42 - SAFIRE aircraft", "abstract": "ATR42-SAFIRE is a large tropospheric research aircraft operated by Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe ATR 42 is a twin-turboprop, short-haul regional airliner built in France and Italy by ATR. The name \"42\" comes from the aircraft's standard seating, which varies from 40 to 52. The ATR-42 320 was designed to have better performance especially in hot and high conditions. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20344, "uuid": "9229a752355a4684b4a6c3b1dbdbe160", "short_code": "instr", "title": "SAFIRE ATR42 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-ATR42 aircraft. Includes Inertial Reference/Navigation System, Non dew/frost point hygrometer, Incident flow vector probe, Dew/Frost-point hygrometer, Global Positioning System, Broad Band Radiometer (x2), Temperature sensor (in situ) and Inertial Reference/Navigation System. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24166, "uuid": "23c3e3d1fb5344e6851848b9349a78fe", "short_code": "acq", "title": "SAFIRE-ATR42 AS46 EUFAR I-WAKE2 Flight, 2010-09-04: data acquisition details", "abstract": "SAFIRE-ATR42 AS46 EUFAR I-WAKE2 Flight, 2010-09-04 data acquisition details." } }, { "ob_id": 11014, "platform": { "ob_id": 11911, "uuid": "8291c6659fb04c0ead2af01941a79c0e", "short_code": "plat", "title": "ATR42 - SAFIRE aircraft", "abstract": "ATR42-SAFIRE is a large tropospheric research aircraft operated by Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe ATR 42 is a twin-turboprop, short-haul regional airliner built in France and Italy by ATR. The name \"42\" comes from the aircraft's standard seating, which varies from 40 to 52. The ATR-42 320 was designed to have better performance especially in hot and high conditions. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20344, "uuid": "9229a752355a4684b4a6c3b1dbdbe160", "short_code": "instr", "title": "SAFIRE ATR42 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-ATR42 aircraft. Includes Inertial Reference/Navigation System, Non dew/frost point hygrometer, Incident flow vector probe, Dew/Frost-point hygrometer, Global Positioning System, Broad Band Radiometer (x2), Temperature sensor (in situ) and Inertial Reference/Navigation System. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24170, "uuid": "bdf9abc42c6b492a811c8a3ee0c3c5d6", "short_code": "acq", "title": "SAFIRE-ATR42 AS47 EUFAR I-WAKE2 Flight, 2010-09-04: data acquisition details", "abstract": "SAFIRE-ATR42 AS47 EUFAR I-WAKE2 Flight, 2010-09-04 data acquisition details." } }, { "ob_id": 11015, "platform": { "ob_id": 11911, "uuid": "8291c6659fb04c0ead2af01941a79c0e", "short_code": "plat", "title": "ATR42 - SAFIRE aircraft", "abstract": "ATR42-SAFIRE is a large tropospheric research aircraft operated by Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe ATR 42 is a twin-turboprop, short-haul regional airliner built in France and Italy by ATR. The name \"42\" comes from the aircraft's standard seating, which varies from 40 to 52. The ATR-42 320 was designed to have better performance especially in hot and high conditions. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20344, "uuid": "9229a752355a4684b4a6c3b1dbdbe160", "short_code": "instr", "title": "SAFIRE ATR42 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-ATR42 aircraft. Includes Inertial Reference/Navigation System, Non dew/frost point hygrometer, Incident flow vector probe, Dew/Frost-point hygrometer, Global Positioning System, Broad Band Radiometer (x2), Temperature sensor (in situ) and Inertial Reference/Navigation System. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24174, "uuid": "2a37c79b7cc640c79091d251f054e1d0", "short_code": "acq", "title": "SAFIRE-ATR42 AS48 EUFAR I-WAKE2 Flight, 2010-09-04: data acquisition details", "abstract": "SAFIRE-ATR42 AS48 EUFAR I-WAKE2 Flight, 2010-09-04 data acquisition details." } }, { "ob_id": 11016, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24178, "uuid": "2fb793e214214bf2b25156fa97c5d024", "short_code": "acq", "title": "KIT-ENDURO EUFAR MORE Flight, 2010-06-13_a: data acquisition details", "abstract": "KIT-ENDURO EUFAR MORE Flight, 2010-06-13_a data acquisition details." } }, { "ob_id": 11017, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24183, "uuid": "5fe5c4aed59049ce98c0d3089520f03d", "short_code": "acq", "title": "KIT-ENDURO EUFAR MORE Flight, 2010-06-15_a: data acquisition details", "abstract": "KIT-ENDURO EUFAR MORE Flight, 2010-06-15_a data acquisition details." } }, { "ob_id": 11018, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24187, "uuid": "c4d9adcfe5f54051bfdf30748b855ec0", "short_code": "acq", "title": "KIT-ENDURO EUFAR MORE Flight, 2010-06-16_a: data acquisition details", "abstract": "KIT-ENDURO EUFAR MORE Flight, 2010-06-16_a data acquisition details." } }, { "ob_id": 11019, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24191, "uuid": "a735970b72d2423787cee4e37d8c8e66", "short_code": "acq", "title": "KIT-ENDURO EUFAR MORE Flight, 2010-06-16_b: data acquisition details", "abstract": "KIT-ENDURO EUFAR MORE Flight, 2010-06-16_b data acquisition details." } }, { "ob_id": 11020, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24195, "uuid": "9ccec844bea642b1abd90ac16f2e5f96", "short_code": "acq", "title": "KIT-ENDURO EUFAR MORE Flight, 2010-06-17_a: data acquisition details", "abstract": "KIT-ENDURO EUFAR MORE Flight, 2010-06-17_a data acquisition details." } }, { "ob_id": 11021, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24199, "uuid": "367017fcd07c4c1e98ac301d5501b720", "short_code": "acq", "title": "KIT-ENDURO EUFAR MORE Flight, 2010-06-17_b: data acquisition details", "abstract": "KIT-ENDURO EUFAR MORE Flight, 2010-06-17_b data acquisition details." } }, { "ob_id": 11022, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24203, "uuid": "ba979c8070ae4c6ea7a6f9471be1d2a3", "short_code": "acq", "title": "KIT-ENDURO EUFAR MORE Flight, 2010-06-19_a: data acquisition details", "abstract": "KIT-ENDURO EUFAR MORE Flight, 2010-06-19_a data acquisition details." } }, { "ob_id": 11023, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24207, "uuid": "ea00a2cb07dd4f66bb498c89de45b8d8", "short_code": "acq", "title": "KIT-ENDURO EUFAR MORE Flight, 2010-06-25_a: data acquisition details", "abstract": "KIT-ENDURO EUFAR MORE Flight, 2010-06-25_a data acquisition details." } }, { "ob_id": 11024, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24211, "uuid": "cf93291a81dd4dbea077c48ff220f82a", "short_code": "acq", "title": "KIT-ENDURO EUFAR MORE Flight, 2010-06-26_a: data acquisition details", "abstract": "KIT-ENDURO EUFAR MORE Flight, 2010-06-26_a data acquisition details." } }, { "ob_id": 11025, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24215, "uuid": "23f763f4a0d64a5aa1cfc56a77d4588f", "short_code": "acq", "title": "KIT-ENDURO EUFAR MORE Flight, 2010-06-26_b: data acquisition details", "abstract": "KIT-ENDURO EUFAR MORE Flight, 2010-06-26_b data acquisition details." } }, { "ob_id": 11026, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24219, "uuid": "96bf13151e3b4391b6072337c02c8a45", "short_code": "acq", "title": "INTACASA-RS EUFAR T-MAPP-FP7 Flight, 2010-07-14: data acquisition details", "abstract": "INTACASA-RS EUFAR T-MAPP-FP7 Flight, 2010-07-14 data acquisition details." } }, { "ob_id": 11027, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24219, "uuid": "96bf13151e3b4391b6072337c02c8a45", "short_code": "acq", "title": "INTACASA-RS EUFAR T-MAPP-FP7 Flight, 2010-07-14: data acquisition details", "abstract": "INTACASA-RS EUFAR T-MAPP-FP7 Flight, 2010-07-14 data acquisition details." } }, { "ob_id": 11028, "platform": { "ob_id": 6387, "uuid": "ca776528e8da4c339d3f3db0b0c3dda3", "short_code": "plat", "title": "POLAR 5 - AWI aircraft", "abstract": "Large tropospheric aircraft operated by Alfred Wegener Institute, Germany. POLAR 5 is a Basler BT-67 type aircraft, a fixed-wing aircraft produced by Basler Turbo Conversions of Oshkosh, Wisconsin. It is built on a retrofitted Douglas DC-3 airframe, with modifications designed to improve the DC-3's serviceable lifetime. The conversion includes fitting the airframe with Pratt & Whitney Canada PT6A-67R turboprop engines, lengthening the fuselage, strengthening the airframe, upgrading the avionics, and making modifications to the wings' leading edge and wing tip. This aricraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20350, "uuid": "a165c29ced4645719b657db72e004916", "short_code": "instr", "title": "Ocean Optics spectrometer on the AWI-polar5 aircraft", "abstract": "Ocean Optics spectrometer onboard the AWI-polar5 aircraft operated by Alfred Wegener Institute. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24238, "uuid": "9f8ed4abfae54a42b24b2b333a532eeb", "short_code": "acq", "title": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-13: data acquisition details", "abstract": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-13 data acquisition details." } }, { "ob_id": 11029, "platform": { "ob_id": 6387, "uuid": "ca776528e8da4c339d3f3db0b0c3dda3", "short_code": "plat", "title": "POLAR 5 - AWI aircraft", "abstract": "Large tropospheric aircraft operated by Alfred Wegener Institute, Germany. POLAR 5 is a Basler BT-67 type aircraft, a fixed-wing aircraft produced by Basler Turbo Conversions of Oshkosh, Wisconsin. It is built on a retrofitted Douglas DC-3 airframe, with modifications designed to improve the DC-3's serviceable lifetime. The conversion includes fitting the airframe with Pratt & Whitney Canada PT6A-67R turboprop engines, lengthening the fuselage, strengthening the airframe, upgrading the avionics, and making modifications to the wings' leading edge and wing tip. This aricraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20349, "uuid": "d2d1bd8806094055bc40f01af8404c64", "short_code": "instr", "title": "AIMMS20 instrument on the AWI-polar5 aircraft", "abstract": "AIMMS20 Instrument onboard the AWI-polar5 aircraft operated by Alfred Wegener Institute. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24238, "uuid": "9f8ed4abfae54a42b24b2b333a532eeb", "short_code": "acq", "title": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-13: data acquisition details", "abstract": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-13 data acquisition details." } }, { "ob_id": 11030, "platform": { "ob_id": 6387, "uuid": "ca776528e8da4c339d3f3db0b0c3dda3", "short_code": "plat", "title": "POLAR 5 - AWI aircraft", "abstract": "Large tropospheric aircraft operated by Alfred Wegener Institute, Germany. POLAR 5 is a Basler BT-67 type aircraft, a fixed-wing aircraft produced by Basler Turbo Conversions of Oshkosh, Wisconsin. It is built on a retrofitted Douglas DC-3 airframe, with modifications designed to improve the DC-3's serviceable lifetime. The conversion includes fitting the airframe with Pratt & Whitney Canada PT6A-67R turboprop engines, lengthening the fuselage, strengthening the airframe, upgrading the avionics, and making modifications to the wings' leading edge and wing tip. This aricraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20350, "uuid": "a165c29ced4645719b657db72e004916", "short_code": "instr", "title": "Ocean Optics spectrometer on the AWI-polar5 aircraft", "abstract": "Ocean Optics spectrometer onboard the AWI-polar5 aircraft operated by Alfred Wegener Institute. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24244, "uuid": "0d9ea5ca41444bb196b9101f3229a913", "short_code": "acq", "title": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-17: data acquisition details", "abstract": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-17 data acquisition details." } }, { "ob_id": 11031, "platform": { "ob_id": 6387, "uuid": "ca776528e8da4c339d3f3db0b0c3dda3", "short_code": "plat", "title": "POLAR 5 - AWI aircraft", "abstract": "Large tropospheric aircraft operated by Alfred Wegener Institute, Germany. POLAR 5 is a Basler BT-67 type aircraft, a fixed-wing aircraft produced by Basler Turbo Conversions of Oshkosh, Wisconsin. It is built on a retrofitted Douglas DC-3 airframe, with modifications designed to improve the DC-3's serviceable lifetime. The conversion includes fitting the airframe with Pratt & Whitney Canada PT6A-67R turboprop engines, lengthening the fuselage, strengthening the airframe, upgrading the avionics, and making modifications to the wings' leading edge and wing tip. This aricraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20349, "uuid": "d2d1bd8806094055bc40f01af8404c64", "short_code": "instr", "title": "AIMMS20 instrument on the AWI-polar5 aircraft", "abstract": "AIMMS20 Instrument onboard the AWI-polar5 aircraft operated by Alfred Wegener Institute. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24244, "uuid": "0d9ea5ca41444bb196b9101f3229a913", "short_code": "acq", "title": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-17: data acquisition details", "abstract": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-17 data acquisition details." } }, { "ob_id": 11032, "platform": { "ob_id": 6387, "uuid": "ca776528e8da4c339d3f3db0b0c3dda3", "short_code": "plat", "title": "POLAR 5 - AWI aircraft", "abstract": "Large tropospheric aircraft operated by Alfred Wegener Institute, Germany. POLAR 5 is a Basler BT-67 type aircraft, a fixed-wing aircraft produced by Basler Turbo Conversions of Oshkosh, Wisconsin. It is built on a retrofitted Douglas DC-3 airframe, with modifications designed to improve the DC-3's serviceable lifetime. The conversion includes fitting the airframe with Pratt & Whitney Canada PT6A-67R turboprop engines, lengthening the fuselage, strengthening the airframe, upgrading the avionics, and making modifications to the wings' leading edge and wing tip. This aricraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20349, "uuid": "d2d1bd8806094055bc40f01af8404c64", "short_code": "instr", "title": "AIMMS20 instrument on the AWI-polar5 aircraft", "abstract": "AIMMS20 Instrument onboard the AWI-polar5 aircraft operated by Alfred Wegener Institute. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24249, "uuid": "192ff5f55a5c494fa334bd30626f29ba", "short_code": "acq", "title": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-27: data acquisition details", "abstract": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-27 data acquisition details." } }, { "ob_id": 11033, "platform": { "ob_id": 6387, "uuid": "ca776528e8da4c339d3f3db0b0c3dda3", "short_code": "plat", "title": "POLAR 5 - AWI aircraft", "abstract": "Large tropospheric aircraft operated by Alfred Wegener Institute, Germany. POLAR 5 is a Basler BT-67 type aircraft, a fixed-wing aircraft produced by Basler Turbo Conversions of Oshkosh, Wisconsin. It is built on a retrofitted Douglas DC-3 airframe, with modifications designed to improve the DC-3's serviceable lifetime. The conversion includes fitting the airframe with Pratt & Whitney Canada PT6A-67R turboprop engines, lengthening the fuselage, strengthening the airframe, upgrading the avionics, and making modifications to the wings' leading edge and wing tip. This aricraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20350, "uuid": "a165c29ced4645719b657db72e004916", "short_code": "instr", "title": "Ocean Optics spectrometer on the AWI-polar5 aircraft", "abstract": "Ocean Optics spectrometer onboard the AWI-polar5 aircraft operated by Alfred Wegener Institute. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24249, "uuid": "192ff5f55a5c494fa334bd30626f29ba", "short_code": "acq", "title": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-27: data acquisition details", "abstract": "AWI-POLAR5 EUFAR ALISA Flight, 2010-02-27 data acquisition details." } }, { "ob_id": 11034, "platform": { "ob_id": 6387, "uuid": "ca776528e8da4c339d3f3db0b0c3dda3", "short_code": "plat", "title": "POLAR 5 - AWI aircraft", "abstract": "Large tropospheric aircraft operated by Alfred Wegener Institute, Germany. POLAR 5 is a Basler BT-67 type aircraft, a fixed-wing aircraft produced by Basler Turbo Conversions of Oshkosh, Wisconsin. It is built on a retrofitted Douglas DC-3 airframe, with modifications designed to improve the DC-3's serviceable lifetime. The conversion includes fitting the airframe with Pratt & Whitney Canada PT6A-67R turboprop engines, lengthening the fuselage, strengthening the airframe, upgrading the avionics, and making modifications to the wings' leading edge and wing tip. This aricraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20349, "uuid": "d2d1bd8806094055bc40f01af8404c64", "short_code": "instr", "title": "AIMMS20 instrument on the AWI-polar5 aircraft", "abstract": "AIMMS20 Instrument onboard the AWI-polar5 aircraft operated by Alfred Wegener Institute. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24254, "uuid": "c67a6adf8a494be7ba70f2e3645b8998", "short_code": "acq", "title": "AWI-POLAR5 EUFAR ALISA Flight, 2010-03-01: data acquisition details", "abstract": "AWI-POLAR5 EUFAR ALISA Flight, 2010-03-01 data acquisition details." } }, { "ob_id": 11035, "platform": { "ob_id": 6387, "uuid": "ca776528e8da4c339d3f3db0b0c3dda3", "short_code": "plat", "title": "POLAR 5 - AWI aircraft", "abstract": "Large tropospheric aircraft operated by Alfred Wegener Institute, Germany. POLAR 5 is a Basler BT-67 type aircraft, a fixed-wing aircraft produced by Basler Turbo Conversions of Oshkosh, Wisconsin. It is built on a retrofitted Douglas DC-3 airframe, with modifications designed to improve the DC-3's serviceable lifetime. The conversion includes fitting the airframe with Pratt & Whitney Canada PT6A-67R turboprop engines, lengthening the fuselage, strengthening the airframe, upgrading the avionics, and making modifications to the wings' leading edge and wing tip. This aricraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20350, "uuid": "a165c29ced4645719b657db72e004916", "short_code": "instr", "title": "Ocean Optics spectrometer on the AWI-polar5 aircraft", "abstract": "Ocean Optics spectrometer onboard the AWI-polar5 aircraft operated by Alfred Wegener Institute. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24254, "uuid": "c67a6adf8a494be7ba70f2e3645b8998", "short_code": "acq", "title": "AWI-POLAR5 EUFAR ALISA Flight, 2010-03-01: data acquisition details", "abstract": "AWI-POLAR5 EUFAR ALISA Flight, 2010-03-01 data acquisition details." } }, { "ob_id": 11036, "platform": { "ob_id": 6387, "uuid": "ca776528e8da4c339d3f3db0b0c3dda3", "short_code": "plat", "title": "POLAR 5 - AWI aircraft", "abstract": "Large tropospheric aircraft operated by Alfred Wegener Institute, Germany. POLAR 5 is a Basler BT-67 type aircraft, a fixed-wing aircraft produced by Basler Turbo Conversions of Oshkosh, Wisconsin. It is built on a retrofitted Douglas DC-3 airframe, with modifications designed to improve the DC-3's serviceable lifetime. The conversion includes fitting the airframe with Pratt & Whitney Canada PT6A-67R turboprop engines, lengthening the fuselage, strengthening the airframe, upgrading the avionics, and making modifications to the wings' leading edge and wing tip. This aricraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20351, "uuid": "7ef0bf75341b4646999dd0f553d4331e", "short_code": "instr", "title": "Ice Radar on the AWI-polar5 aircraft", "abstract": "Ice Radar (AWi Radio-Echo Sounding system) onboard the AWI-polar5 aircraft operated by Alfred Wegener Institute. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24259, "uuid": "e6cd586c39084bad9d59a8a961ca53c2", "short_code": "acq", "title": "AWI-POLAR5 EUFAR SRMGLACIERS Flight, 2011-01-21: data acquisition details", "abstract": "AWI-POLAR5 EUFAR SRMGLACIERS Flight, 2011-01-21 data acquisition details." } }, { "ob_id": 11037, "platform": { "ob_id": 6387, "uuid": "ca776528e8da4c339d3f3db0b0c3dda3", "short_code": "plat", "title": "POLAR 5 - AWI aircraft", "abstract": "Large tropospheric aircraft operated by Alfred Wegener Institute, Germany. POLAR 5 is a Basler BT-67 type aircraft, a fixed-wing aircraft produced by Basler Turbo Conversions of Oshkosh, Wisconsin. It is built on a retrofitted Douglas DC-3 airframe, with modifications designed to improve the DC-3's serviceable lifetime. The conversion includes fitting the airframe with Pratt & Whitney Canada PT6A-67R turboprop engines, lengthening the fuselage, strengthening the airframe, upgrading the avionics, and making modifications to the wings' leading edge and wing tip. This aricraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20351, "uuid": "7ef0bf75341b4646999dd0f553d4331e", "short_code": "instr", "title": "Ice Radar on the AWI-polar5 aircraft", "abstract": "Ice Radar (AWi Radio-Echo Sounding system) onboard the AWI-polar5 aircraft operated by Alfred Wegener Institute. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24265, "uuid": "ec668ff268954f8390b7a0fee50bcedf", "short_code": "acq", "title": "AWI-POLAR5 EUFAR SRMGLACIERS Flight, 2011-01-22: data acquisition details", "abstract": "AWI-POLAR5 EUFAR SRMGLACIERS Flight, 2011-01-22 data acquisition details." } }, { "ob_id": 11038, "platform": { "ob_id": 6387, "uuid": "ca776528e8da4c339d3f3db0b0c3dda3", "short_code": "plat", "title": "POLAR 5 - AWI aircraft", "abstract": "Large tropospheric aircraft operated by Alfred Wegener Institute, Germany. POLAR 5 is a Basler BT-67 type aircraft, a fixed-wing aircraft produced by Basler Turbo Conversions of Oshkosh, Wisconsin. It is built on a retrofitted Douglas DC-3 airframe, with modifications designed to improve the DC-3's serviceable lifetime. The conversion includes fitting the airframe with Pratt & Whitney Canada PT6A-67R turboprop engines, lengthening the fuselage, strengthening the airframe, upgrading the avionics, and making modifications to the wings' leading edge and wing tip. This aricraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20351, "uuid": "7ef0bf75341b4646999dd0f553d4331e", "short_code": "instr", "title": "Ice Radar on the AWI-polar5 aircraft", "abstract": "Ice Radar (AWi Radio-Echo Sounding system) onboard the AWI-polar5 aircraft operated by Alfred Wegener Institute. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24270, "uuid": "cbb5729fc755496d94add4a4c47ff0a3", "short_code": "acq", "title": "AWI-POLAR5 EUFAR SRMGLACIERS Flight, 2011-01-23: data acquisition details", "abstract": "AWI-POLAR5 EUFAR SRMGLACIERS Flight, 2011-01-23 data acquisition details." } }, { "ob_id": 11039, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24274, "uuid": "cc2901e96f85461b8e7e824be7cfedd5", "short_code": "acq", "title": "INTACASA-RS EUFAR VALCALHYP Flight, 2010-10-28: data acquisition details", "abstract": "INTACASA-RS EUFAR VALCALHYP Flight, 2010-10-28 data acquisition details." } }, { "ob_id": 11040, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24274, "uuid": "cc2901e96f85461b8e7e824be7cfedd5", "short_code": "acq", "title": "INTACASA-RS EUFAR VALCALHYP Flight, 2010-10-28: data acquisition details", "abstract": "INTACASA-RS EUFAR VALCALHYP Flight, 2010-10-28 data acquisition details." } }, { "ob_id": 11041, "platform": { "ob_id": 6392, "uuid": "2642ba3066d24796979e4bfb8dfa7ef8", "short_code": "plat", "title": "PIPER AZTEC - SAFIRE aircraft", "abstract": "PIPER AZTEC - SAFIRE is a small tropospheric research aircraft (PA23-250 type) operated by the Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe Piper PA-23 aircraft is a 1950s American twin-engined monoplane. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20346, "uuid": "21d2c7035d3e476f9bbbf6af07c007c7", "short_code": "instr", "title": "SAFIRE Piper-Aztec Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-Piper-Aztec aircraft. Includes Incident flow vector probe, Non Dew/Frost-point hygrometer, Radio Altimeter, Static Pressure(Rosemount) and Temperature sensor (in situ)(Rosemount). Other optional instruments may be operated. Used in EUFAR flights. " }, "relatedTo": { "ob_id": 24279, "uuid": "e4b73972762c404e9e73cfebdb135517", "short_code": "acq", "title": "SAFIRE-PIPER-AZTEC AZ08 EUFAR BLLATE1 Flight, 2011-06-19 iop2: data acquisition details", "abstract": "SAFIRE-PIPER-AZTEC AZ08 EUFAR BLLATE1 Flight, 2011-06-19 iop2 data acquisition details." } }, { "ob_id": 11042, "platform": { "ob_id": 6392, "uuid": "2642ba3066d24796979e4bfb8dfa7ef8", "short_code": "plat", "title": "PIPER AZTEC - SAFIRE aircraft", "abstract": "PIPER AZTEC - SAFIRE is a small tropospheric research aircraft (PA23-250 type) operated by the Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe Piper PA-23 aircraft is a 1950s American twin-engined monoplane. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20346, "uuid": "21d2c7035d3e476f9bbbf6af07c007c7", "short_code": "instr", "title": "SAFIRE Piper-Aztec Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-Piper-Aztec aircraft. Includes Incident flow vector probe, Non Dew/Frost-point hygrometer, Radio Altimeter, Static Pressure(Rosemount) and Temperature sensor (in situ)(Rosemount). Other optional instruments may be operated. Used in EUFAR flights. " }, "relatedTo": { "ob_id": 24284, "uuid": "a06446a9bf6a45d8b5f784cf8c5662a1", "short_code": "acq", "title": "SAFIRE-PIPER-AZTEC AZ06 EUFAR BLLATE1 Flight, 2011-06-15 iop1: data acquisition details", "abstract": "SAFIRE-PIPER-AZTEC AZ06 EUFAR BLLATE1 Flight, 2011-06-15 iop1 data acquisition details." } }, { "ob_id": 11043, "platform": { "ob_id": 6392, "uuid": "2642ba3066d24796979e4bfb8dfa7ef8", "short_code": "plat", "title": "PIPER AZTEC - SAFIRE aircraft", "abstract": "PIPER AZTEC - SAFIRE is a small tropospheric research aircraft (PA23-250 type) operated by the Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe Piper PA-23 aircraft is a 1950s American twin-engined monoplane. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20346, "uuid": "21d2c7035d3e476f9bbbf6af07c007c7", "short_code": "instr", "title": "SAFIRE Piper-Aztec Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-Piper-Aztec aircraft. Includes Incident flow vector probe, Non Dew/Frost-point hygrometer, Radio Altimeter, Static Pressure(Rosemount) and Temperature sensor (in situ)(Rosemount). Other optional instruments may be operated. Used in EUFAR flights. " }, "relatedTo": { "ob_id": 24288, "uuid": "7b5f11d3e91d4a6a820250aee55b8579", "short_code": "acq", "title": "SAFIRE-PIPER-AZTEC AZ10 EUFAR BLLATE1 Flight, 2011-06-20 iop3: data acquisition details", "abstract": "SAFIRE-PIPER-AZTEC AZ10 EUFAR BLLATE1 Flight, 2011-06-20 iop3 data acquisition details." } }, { "ob_id": 11044, "platform": { "ob_id": 6392, "uuid": "2642ba3066d24796979e4bfb8dfa7ef8", "short_code": "plat", "title": "PIPER AZTEC - SAFIRE aircraft", "abstract": "PIPER AZTEC - SAFIRE is a small tropospheric research aircraft (PA23-250 type) operated by the Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe Piper PA-23 aircraft is a 1950s American twin-engined monoplane. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20346, "uuid": "21d2c7035d3e476f9bbbf6af07c007c7", "short_code": "instr", "title": "SAFIRE Piper-Aztec Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-Piper-Aztec aircraft. Includes Incident flow vector probe, Non Dew/Frost-point hygrometer, Radio Altimeter, Static Pressure(Rosemount) and Temperature sensor (in situ)(Rosemount). Other optional instruments may be operated. Used in EUFAR flights. " }, "relatedTo": { "ob_id": 24292, "uuid": "c1dbc90aa5f149628dd57b1104c022a5", "short_code": "acq", "title": "SAFIRE-PIPER-AZTEC AZ07 EUFAR BLLATE1 Flight, 2011-06-15 iop1: data acquisition details", "abstract": "SAFIRE-PIPER-AZTEC AZ07 EUFAR BLLATE1 Flight, 2011-06-15 iop1 data acquisition details." } }, { "ob_id": 11045, "platform": { "ob_id": 6392, "uuid": "2642ba3066d24796979e4bfb8dfa7ef8", "short_code": "plat", "title": "PIPER AZTEC - SAFIRE aircraft", "abstract": "PIPER AZTEC - SAFIRE is a small tropospheric research aircraft (PA23-250 type) operated by the Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe Piper PA-23 aircraft is a 1950s American twin-engined monoplane. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20346, "uuid": "21d2c7035d3e476f9bbbf6af07c007c7", "short_code": "instr", "title": "SAFIRE Piper-Aztec Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-Piper-Aztec aircraft. Includes Incident flow vector probe, Non Dew/Frost-point hygrometer, Radio Altimeter, Static Pressure(Rosemount) and Temperature sensor (in situ)(Rosemount). Other optional instruments may be operated. Used in EUFAR flights. " }, "relatedTo": { "ob_id": 24296, "uuid": "93a5539764824102b854be3de6b4f276", "short_code": "acq", "title": "SAFIRE-PIPER-AZTEC AZ09 EUFAR BLLATE1 Flight, 2011-06-19 iop2: data acquisition details", "abstract": "SAFIRE-PIPER-AZTEC AZ09 EUFAR BLLATE1 Flight, 2011-06-19 iop2 data acquisition details." } }, { "ob_id": 11046, "platform": { "ob_id": 6392, "uuid": "2642ba3066d24796979e4bfb8dfa7ef8", "short_code": "plat", "title": "PIPER AZTEC - SAFIRE aircraft", "abstract": "PIPER AZTEC - SAFIRE is a small tropospheric research aircraft (PA23-250 type) operated by the Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe Piper PA-23 aircraft is a 1950s American twin-engined monoplane. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20346, "uuid": "21d2c7035d3e476f9bbbf6af07c007c7", "short_code": "instr", "title": "SAFIRE Piper-Aztec Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-Piper-Aztec aircraft. Includes Incident flow vector probe, Non Dew/Frost-point hygrometer, Radio Altimeter, Static Pressure(Rosemount) and Temperature sensor (in situ)(Rosemount). Other optional instruments may be operated. Used in EUFAR flights. " }, "relatedTo": { "ob_id": 24300, "uuid": "e4497ba6dac149f0985437d16a0e828a", "short_code": "acq", "title": "SAFIRE-PIPER-AZTEC AZ11 EUFAR BLLATE1 Flight, 2011-06-20 iop3: data acquisition details", "abstract": "SAFIRE-PIPER-AZTEC AZ11 EUFAR BLLATE1 Flight, 2011-06-20 iop3 data acquisition details." } }, { "ob_id": 11047, "platform": { "ob_id": 6392, "uuid": "2642ba3066d24796979e4bfb8dfa7ef8", "short_code": "plat", "title": "PIPER AZTEC - SAFIRE aircraft", "abstract": "PIPER AZTEC - SAFIRE is a small tropospheric research aircraft (PA23-250 type) operated by the Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe Piper PA-23 aircraft is a 1950s American twin-engined monoplane. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20346, "uuid": "21d2c7035d3e476f9bbbf6af07c007c7", "short_code": "instr", "title": "SAFIRE Piper-Aztec Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-Piper-Aztec aircraft. Includes Incident flow vector probe, Non Dew/Frost-point hygrometer, Radio Altimeter, Static Pressure(Rosemount) and Temperature sensor (in situ)(Rosemount). Other optional instruments may be operated. Used in EUFAR flights. " }, "relatedTo": { "ob_id": 24304, "uuid": "1d5a240f5d994b569cff6b530139f3fb", "short_code": "acq", "title": "SAFIRE-PIPER-AZTEC AZ14 EUFAR BLLATE1 Flight, 2011-06-25 iop5: data acquisition details", "abstract": "SAFIRE-PIPER-AZTEC AZ14 EUFAR BLLATE1 Flight, 2011-06-25 iop5 data acquisition details." } }, { "ob_id": 11048, "platform": { "ob_id": 6392, "uuid": "2642ba3066d24796979e4bfb8dfa7ef8", "short_code": "plat", "title": "PIPER AZTEC - SAFIRE aircraft", "abstract": "PIPER AZTEC - SAFIRE is a small tropospheric research aircraft (PA23-250 type) operated by the Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe Piper PA-23 aircraft is a 1950s American twin-engined monoplane. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20346, "uuid": "21d2c7035d3e476f9bbbf6af07c007c7", "short_code": "instr", "title": "SAFIRE Piper-Aztec Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-Piper-Aztec aircraft. Includes Incident flow vector probe, Non Dew/Frost-point hygrometer, Radio Altimeter, Static Pressure(Rosemount) and Temperature sensor (in situ)(Rosemount). Other optional instruments may be operated. Used in EUFAR flights. " }, "relatedTo": { "ob_id": 24308, "uuid": "15eefbd020764196abed2c3dd0b618d6", "short_code": "acq", "title": "SAFIRE-PIPER-AZTEC AZ12 EUFAR BLLATE1 Flight, 2011-06-25 iop5: data acquisition details", "abstract": "SAFIRE-PIPER-AZTEC AZ12 EUFAR BLLATE1 Flight, 2011-06-25 iop5 data acquisition details." } }, { "ob_id": 11049, "platform": { "ob_id": 6391, "uuid": "94149b5f90744b77a4149aa180d35de6", "short_code": "plat", "title": "ERA SkyArrow-IBIMET aircraft", "abstract": "The Environmental Aircraft (ERA) SkyArrow-IBIMET is a small tropospheric aircraft operated by the Institute of Biometeorology, Italy. \r\nThe Sky Arrow features a strong, lightweight all carbon-fiber airframe and is powered by a 100 HP pusher engine. It is equipped with a fixed pitch propeller, a rectangular wing supported by two struts, and a fixed landing gear. Its maximum flight speed is 105 knots, with a low stall speed of 35 knots.\r\n\r\nThe 650 ERA has a gross weight of 650 kg. This model has hard points, portholes and power capabilities to accommodate the ATDD BAT probe and MFP system mounting and power requirements. The aircraft is especially suited for high-fidelity flux measurements at 70 knots flight speed and altitudes up to 12,000 ft MSL." }, "instrument": { "ob_id": 20347, "uuid": "ccb4b8adb9564145a67c4a7f3a4fff4a", "short_code": "instr", "title": "ERA SkyArrow IBIMET core instruments", "abstract": "Instruments onboard the \tERA SkyArrow IBIMET aircraft operated by IBIMET (CNR-Institute of Biometeorology). May include: Incident flow vector probe, CO2 and H20 by InfraRed absorption, Visible/Near Infra Red Spectrometer depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24312, "uuid": "a30fc1d011324816bb86746489d322e3", "short_code": "acq", "title": "SKYARROW EUFAR BLLATE2 Flight, 2011-06-15 iop1: data acquisition details", "abstract": "SKYARROW EUFAR BLLATE2 Flight, 2011-06-15 iop1 data acquisition details." } }, { "ob_id": 11050, "platform": { "ob_id": 6391, "uuid": "94149b5f90744b77a4149aa180d35de6", "short_code": "plat", "title": "ERA SkyArrow-IBIMET aircraft", "abstract": "The Environmental Aircraft (ERA) SkyArrow-IBIMET is a small tropospheric aircraft operated by the Institute of Biometeorology, Italy. \r\nThe Sky Arrow features a strong, lightweight all carbon-fiber airframe and is powered by a 100 HP pusher engine. It is equipped with a fixed pitch propeller, a rectangular wing supported by two struts, and a fixed landing gear. Its maximum flight speed is 105 knots, with a low stall speed of 35 knots.\r\n\r\nThe 650 ERA has a gross weight of 650 kg. This model has hard points, portholes and power capabilities to accommodate the ATDD BAT probe and MFP system mounting and power requirements. The aircraft is especially suited for high-fidelity flux measurements at 70 knots flight speed and altitudes up to 12,000 ft MSL." }, "instrument": { "ob_id": 20347, "uuid": "ccb4b8adb9564145a67c4a7f3a4fff4a", "short_code": "instr", "title": "ERA SkyArrow IBIMET core instruments", "abstract": "Instruments onboard the \tERA SkyArrow IBIMET aircraft operated by IBIMET (CNR-Institute of Biometeorology). May include: Incident flow vector probe, CO2 and H20 by InfraRed absorption, Visible/Near Infra Red Spectrometer depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24317, "uuid": "2d25f1fbb21e4afd82c7b932239ea13a", "short_code": "acq", "title": "SKYARROW EUFAR BLLATE2 Flight, 2011-06-19 iop2: data acquisition details", "abstract": "SKYARROW EUFAR BLLATE2 Flight, 2011-06-19 iop2 data acquisition details." } }, { "ob_id": 11051, "platform": { "ob_id": 6391, "uuid": "94149b5f90744b77a4149aa180d35de6", "short_code": "plat", "title": "ERA SkyArrow-IBIMET aircraft", "abstract": "The Environmental Aircraft (ERA) SkyArrow-IBIMET is a small tropospheric aircraft operated by the Institute of Biometeorology, Italy. \r\nThe Sky Arrow features a strong, lightweight all carbon-fiber airframe and is powered by a 100 HP pusher engine. It is equipped with a fixed pitch propeller, a rectangular wing supported by two struts, and a fixed landing gear. Its maximum flight speed is 105 knots, with a low stall speed of 35 knots.\r\n\r\nThe 650 ERA has a gross weight of 650 kg. This model has hard points, portholes and power capabilities to accommodate the ATDD BAT probe and MFP system mounting and power requirements. The aircraft is especially suited for high-fidelity flux measurements at 70 knots flight speed and altitudes up to 12,000 ft MSL." }, "instrument": { "ob_id": 20347, "uuid": "ccb4b8adb9564145a67c4a7f3a4fff4a", "short_code": "instr", "title": "ERA SkyArrow IBIMET core instruments", "abstract": "Instruments onboard the \tERA SkyArrow IBIMET aircraft operated by IBIMET (CNR-Institute of Biometeorology). May include: Incident flow vector probe, CO2 and H20 by InfraRed absorption, Visible/Near Infra Red Spectrometer depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24321, "uuid": "2d37e8f831084592afef45b05b9d86ed", "short_code": "acq", "title": "SKYARROW EUFAR BLLATE2 Flight, 2011-06-20 iop3: data acquisition details", "abstract": "SKYARROW EUFAR BLLATE2 Flight, 2011-06-20 iop3 data acquisition details." } }, { "ob_id": 11052, "platform": { "ob_id": 6391, "uuid": "94149b5f90744b77a4149aa180d35de6", "short_code": "plat", "title": "ERA SkyArrow-IBIMET aircraft", "abstract": "The Environmental Aircraft (ERA) SkyArrow-IBIMET is a small tropospheric aircraft operated by the Institute of Biometeorology, Italy. \r\nThe Sky Arrow features a strong, lightweight all carbon-fiber airframe and is powered by a 100 HP pusher engine. It is equipped with a fixed pitch propeller, a rectangular wing supported by two struts, and a fixed landing gear. Its maximum flight speed is 105 knots, with a low stall speed of 35 knots.\r\n\r\nThe 650 ERA has a gross weight of 650 kg. This model has hard points, portholes and power capabilities to accommodate the ATDD BAT probe and MFP system mounting and power requirements. The aircraft is especially suited for high-fidelity flux measurements at 70 knots flight speed and altitudes up to 12,000 ft MSL." }, "instrument": { "ob_id": 20347, "uuid": "ccb4b8adb9564145a67c4a7f3a4fff4a", "short_code": "instr", "title": "ERA SkyArrow IBIMET core instruments", "abstract": "Instruments onboard the \tERA SkyArrow IBIMET aircraft operated by IBIMET (CNR-Institute of Biometeorology). May include: Incident flow vector probe, CO2 and H20 by InfraRed absorption, Visible/Near Infra Red Spectrometer depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24325, "uuid": "a3185f17b7ed4810812c7bba91df6f3c", "short_code": "acq", "title": "SKYARROW EUFAR BLLATE2 Flight, 2011-06-24 iop4: data acquisition details", "abstract": "SKYARROW EUFAR BLLATE2 Flight, 2011-06-24 iop4 data acquisition details." } }, { "ob_id": 11053, "platform": { "ob_id": 6391, "uuid": "94149b5f90744b77a4149aa180d35de6", "short_code": "plat", "title": "ERA SkyArrow-IBIMET aircraft", "abstract": "The Environmental Aircraft (ERA) SkyArrow-IBIMET is a small tropospheric aircraft operated by the Institute of Biometeorology, Italy. \r\nThe Sky Arrow features a strong, lightweight all carbon-fiber airframe and is powered by a 100 HP pusher engine. It is equipped with a fixed pitch propeller, a rectangular wing supported by two struts, and a fixed landing gear. Its maximum flight speed is 105 knots, with a low stall speed of 35 knots.\r\n\r\nThe 650 ERA has a gross weight of 650 kg. This model has hard points, portholes and power capabilities to accommodate the ATDD BAT probe and MFP system mounting and power requirements. The aircraft is especially suited for high-fidelity flux measurements at 70 knots flight speed and altitudes up to 12,000 ft MSL." }, "instrument": { "ob_id": 20347, "uuid": "ccb4b8adb9564145a67c4a7f3a4fff4a", "short_code": "instr", "title": "ERA SkyArrow IBIMET core instruments", "abstract": "Instruments onboard the \tERA SkyArrow IBIMET aircraft operated by IBIMET (CNR-Institute of Biometeorology). May include: Incident flow vector probe, CO2 and H20 by InfraRed absorption, Visible/Near Infra Red Spectrometer depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24329, "uuid": "557c4c1a6ab54d059d6baba3e23d446c", "short_code": "acq", "title": "SKYARROW EUFAR BLLATE2 Flight, 2011-06-25 iop5: data acquisition details", "abstract": "SKYARROW EUFAR BLLATE2 Flight, 2011-06-25 iop5 data acquisition details." } }, { "ob_id": 11054, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24333, "uuid": "f94e457ac40f44458b147d3e022fecd3", "short_code": "acq", "title": "INTACASA-RS EUFAR DEMINTIR Flight, 2011-07-19: data acquisition details", "abstract": "INTACASA-RS EUFAR DEMINTIR Flight, 2011-07-19 data acquisition details." } }, { "ob_id": 11055, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24333, "uuid": "f94e457ac40f44458b147d3e022fecd3", "short_code": "acq", "title": "INTACASA-RS EUFAR DEMINTIR Flight, 2011-07-19: data acquisition details", "abstract": "INTACASA-RS EUFAR DEMINTIR Flight, 2011-07-19 data acquisition details." } }, { "ob_id": 11056, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24338, "uuid": "ad2f469f62804769acbd46818125f144", "short_code": "acq", "title": "INTACASA-RS EUFAR DEMINTIR Flight, 2011-07-22: data acquisition details", "abstract": "INTACASA-RS EUFAR DEMINTIR Flight, 2011-07-22 data acquisition details." } }, { "ob_id": 11057, "platform": { "ob_id": 6389, "uuid": "23cc5b5b39a346cc80b98841da22d46e", "short_code": "plat", "title": "DO228-212 /D-CFFU - DLR aircraft", "abstract": "Medium tropospheric aircraft operated by Deutsches Zentrum fur Luft- und Raumfahrt e.V., Germany.\r\n\r\nThe Dornier 228 is a twin-turboprop STOL (short take-off and landing) utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier) from 1981 until 1998. This aircraft is part of the EUFAR fleet." }, "instrument": { "ob_id": 20354, "uuid": "add62b7ab00944999da4f0c973c858e8", "short_code": "instr", "title": "Airborne Prism Experiment (APEX)", "abstract": "The Airborne Prism Experiment (APEX) instrument is a hyperspectral remote sensing imaging spectrometer developed by a Swiss-Belgian consortium on behalf of ESA. It is being operated jointly by VITO Centre for Remote Sensing (Belgium) and RSL (Switzerland). http://www.apex-esa.org/. APEX is a dispersive pushbroom imaging spectrometer covering the solar reflected wavelength range between 372 and 2540 nm with nominal 312 (max. 532) spectral bands. APEX is calibrated using a combination of laboratory, in-flight and vicarious calibration approaches. These are complemented by using a forward and inverse radiative transfer modeling approach, suitable to further validate APEX data. It is flown on board the DLR dornier aircraft during EUFAR flights." }, "relatedTo": { "ob_id": 24342, "uuid": "9144913077c6433ebefe4a834caeb4a3", "short_code": "acq", "title": "APEX EUFAR HABLAKES Flight, 2011-09-21 day2: data acquisition details", "abstract": "APEX EUFAR HABLAKES Flight, 2011-09-21 day2 data acquisition details." } }, { "ob_id": 11058, "platform": { "ob_id": 6389, "uuid": "23cc5b5b39a346cc80b98841da22d46e", "short_code": "plat", "title": "DO228-212 /D-CFFU - DLR aircraft", "abstract": "Medium tropospheric aircraft operated by Deutsches Zentrum fur Luft- und Raumfahrt e.V., Germany.\r\n\r\nThe Dornier 228 is a twin-turboprop STOL (short take-off and landing) utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier) from 1981 until 1998. This aircraft is part of the EUFAR fleet." }, "instrument": { "ob_id": 20354, "uuid": "add62b7ab00944999da4f0c973c858e8", "short_code": "instr", "title": "Airborne Prism Experiment (APEX)", "abstract": "The Airborne Prism Experiment (APEX) instrument is a hyperspectral remote sensing imaging spectrometer developed by a Swiss-Belgian consortium on behalf of ESA. It is being operated jointly by VITO Centre for Remote Sensing (Belgium) and RSL (Switzerland). http://www.apex-esa.org/. APEX is a dispersive pushbroom imaging spectrometer covering the solar reflected wavelength range between 372 and 2540 nm with nominal 312 (max. 532) spectral bands. APEX is calibrated using a combination of laboratory, in-flight and vicarious calibration approaches. These are complemented by using a forward and inverse radiative transfer modeling approach, suitable to further validate APEX data. It is flown on board the DLR dornier aircraft during EUFAR flights." }, "relatedTo": { "ob_id": 24347, "uuid": "cfa4a1990ff14a5aa01f0ef6ae97752f", "short_code": "acq", "title": "APEX EUFAR HABLAKES Flight, 2011-09-09 day1: data acquisition details", "abstract": "APEX EUFAR HABLAKES Flight, 2011-09-09 day1 data acquisition details." } }, { "ob_id": 11059, "platform": { "ob_id": 6389, "uuid": "23cc5b5b39a346cc80b98841da22d46e", "short_code": "plat", "title": "DO228-212 /D-CFFU - DLR aircraft", "abstract": "Medium tropospheric aircraft operated by Deutsches Zentrum fur Luft- und Raumfahrt e.V., Germany.\r\n\r\nThe Dornier 228 is a twin-turboprop STOL (short take-off and landing) utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier) from 1981 until 1998. This aircraft is part of the EUFAR fleet." }, "instrument": { "ob_id": 20354, "uuid": "add62b7ab00944999da4f0c973c858e8", "short_code": "instr", "title": "Airborne Prism Experiment (APEX)", "abstract": "The Airborne Prism Experiment (APEX) instrument is a hyperspectral remote sensing imaging spectrometer developed by a Swiss-Belgian consortium on behalf of ESA. It is being operated jointly by VITO Centre for Remote Sensing (Belgium) and RSL (Switzerland). http://www.apex-esa.org/. APEX is a dispersive pushbroom imaging spectrometer covering the solar reflected wavelength range between 372 and 2540 nm with nominal 312 (max. 532) spectral bands. APEX is calibrated using a combination of laboratory, in-flight and vicarious calibration approaches. These are complemented by using a forward and inverse radiative transfer modeling approach, suitable to further validate APEX data. It is flown on board the DLR dornier aircraft during EUFAR flights." }, "relatedTo": { "ob_id": 24351, "uuid": "23a5f022255342f7953deba64d41757a", "short_code": "acq", "title": "APEX EUFAR HYPERSTRESS Flight, 2011-09-08: data acquisition details", "abstract": "APEX EUFAR HYPERSTRESS Flight, 2011-09-08 data acquisition details." } }, { "ob_id": 11060, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24357, "uuid": "8cd93a6609f04dec85c423b63d5e6624", "short_code": "acq", "title": "INTACASA-RS EUFAR IMROM Flight, 2011-07-25: data acquisition details", "abstract": "INTACASA-RS EUFAR IMROM Flight, 2011-07-25 data acquisition details." } }, { "ob_id": 11061, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24357, "uuid": "8cd93a6609f04dec85c423b63d5e6624", "short_code": "acq", "title": "INTACASA-RS EUFAR IMROM Flight, 2011-07-25: data acquisition details", "abstract": "INTACASA-RS EUFAR IMROM Flight, 2011-07-25 data acquisition details." } }, { "ob_id": 11062, "platform": { "ob_id": 6389, "uuid": "23cc5b5b39a346cc80b98841da22d46e", "short_code": "plat", "title": "DO228-212 /D-CFFU - DLR aircraft", "abstract": "Medium tropospheric aircraft operated by Deutsches Zentrum fur Luft- und Raumfahrt e.V., Germany.\r\n\r\nThe Dornier 228 is a twin-turboprop STOL (short take-off and landing) utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier) from 1981 until 1998. This aircraft is part of the EUFAR fleet." }, "instrument": { "ob_id": 20354, "uuid": "add62b7ab00944999da4f0c973c858e8", "short_code": "instr", "title": "Airborne Prism Experiment (APEX)", "abstract": "The Airborne Prism Experiment (APEX) instrument is a hyperspectral remote sensing imaging spectrometer developed by a Swiss-Belgian consortium on behalf of ESA. It is being operated jointly by VITO Centre for Remote Sensing (Belgium) and RSL (Switzerland). http://www.apex-esa.org/. APEX is a dispersive pushbroom imaging spectrometer covering the solar reflected wavelength range between 372 and 2540 nm with nominal 312 (max. 532) spectral bands. APEX is calibrated using a combination of laboratory, in-flight and vicarious calibration approaches. These are complemented by using a forward and inverse radiative transfer modeling approach, suitable to further validate APEX data. It is flown on board the DLR dornier aircraft during EUFAR flights." }, "relatedTo": { "ob_id": 24362, "uuid": "a26b49a13d1c4ba5a2f28cd252d91941", "short_code": "acq", "title": "APEX EUFAR HYPPOS Flight, 2014-09-27: data acquisition details", "abstract": "APEX EUFAR HYPPOS Flight, 2014-09-27 data acquisition details." } }, { "ob_id": 11063, "platform": { "ob_id": 6398, "uuid": "32ce062fe89a4c1eb8ab3e67c1f9ad45", "short_code": "plat", "title": "FA20 - SAFIRE aircraft", "abstract": "FA20 - SAFIRE is a large tropospheric research aircraft (ATR42-320 type) operated by the Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France. This aircraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20345, "uuid": "b1f5d0b1910f4aa0943f009886940507", "short_code": "instr", "title": "SAFIRE Falcon20 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-Falcon20 aircraft. Includes Inertial Reference/Navigation System, Incident flow vector probe, Dew/Frost-point hygrometer (Buck and General Eastern), and AVAPS Dropsonde. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24367, "uuid": "64eb2f8bcf614e13b3f4c1f51cb299c6", "short_code": "acq", "title": "SAFIRE-FA20 FS13 EUFAR RAIN4DUST Flight, 2011-06-11: data acquisition details", "abstract": "SAFIRE-FA20 FS13 EUFAR RAIN4DUST Flight, 2011-06-11 data acquisition details." } }, { "ob_id": 11064, "platform": { "ob_id": 6398, "uuid": "32ce062fe89a4c1eb8ab3e67c1f9ad45", "short_code": "plat", "title": "FA20 - SAFIRE aircraft", "abstract": "FA20 - SAFIRE is a large tropospheric research aircraft (ATR42-320 type) operated by the Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France. This aircraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20345, "uuid": "b1f5d0b1910f4aa0943f009886940507", "short_code": "instr", "title": "SAFIRE Falcon20 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-Falcon20 aircraft. Includes Inertial Reference/Navigation System, Incident flow vector probe, Dew/Frost-point hygrometer (Buck and General Eastern), and AVAPS Dropsonde. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24372, "uuid": "534759f8e6234a65925fed359976880a", "short_code": "acq", "title": "SAFIRE-FA20 FS18 EUFAR RAIN4DUST Flight, 2011-06-16: data acquisition details", "abstract": "SAFIRE-FA20 FS18 EUFAR RAIN4DUST Flight, 2011-06-16 data acquisition details." } }, { "ob_id": 11065, "platform": { "ob_id": 6398, "uuid": "32ce062fe89a4c1eb8ab3e67c1f9ad45", "short_code": "plat", "title": "FA20 - SAFIRE aircraft", "abstract": "FA20 - SAFIRE is a large tropospheric research aircraft (ATR42-320 type) operated by the Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France. This aircraft is part of the EUFAR TA fleet." }, "instrument": { "ob_id": 20345, "uuid": "b1f5d0b1910f4aa0943f009886940507", "short_code": "instr", "title": "SAFIRE Falcon20 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-Falcon20 aircraft. Includes Inertial Reference/Navigation System, Incident flow vector probe, Dew/Frost-point hygrometer (Buck and General Eastern), and AVAPS Dropsonde. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24376, "uuid": "ccd1cf714d164dc6a4131da9de318148", "short_code": "acq", "title": "SAFIRE-FA20 FS26 EUFAR RAIN4DUST Flight, 2011-06-23: data acquisition details", "abstract": "SAFIRE-FA20 FS26 EUFAR RAIN4DUST Flight, 2011-06-23 data acquisition details." } }, { "ob_id": 11066, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24380, "uuid": "eca8b82567ec4e148a812645061c88f0", "short_code": "acq", "title": "INTACASA-RS EUFAR UR-TIR Flight, 2011-07-05: data acquisition details", "abstract": "INTACASA-RS EUFAR UR-TIR Flight, 2011-07-05 data acquisition details." } }, { "ob_id": 11067, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24380, "uuid": "eca8b82567ec4e148a812645061c88f0", "short_code": "acq", "title": "INTACASA-RS EUFAR UR-TIR Flight, 2011-07-05: data acquisition details", "abstract": "INTACASA-RS EUFAR UR-TIR Flight, 2011-07-05 data acquisition details." } }, { "ob_id": 11068, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24385, "uuid": "e297698a6b2643a5bcf1c3cedef0ce56", "short_code": "acq", "title": "INTACASA-RS EUFAR UR-TIR Flight, 2011-07-12: data acquisition details", "abstract": "INTACASA-RS EUFAR UR-TIR Flight, 2011-07-12 data acquisition details." } }, { "ob_id": 11069, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24385, "uuid": "e297698a6b2643a5bcf1c3cedef0ce56", "short_code": "acq", "title": "INTACASA-RS EUFAR UR-TIR Flight, 2011-07-12: data acquisition details", "abstract": "INTACASA-RS EUFAR UR-TIR Flight, 2011-07-12 data acquisition details." } }, { "ob_id": 11070, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24389, "uuid": "9f0ca3b9c6c34cc3b8b3f94ddfaa8a3f", "short_code": "acq", "title": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-04 BU: data acquisition details", "abstract": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-04 BU data acquisition details." } }, { "ob_id": 11071, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24389, "uuid": "9f0ca3b9c6c34cc3b8b3f94ddfaa8a3f", "short_code": "acq", "title": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-04 BU: data acquisition details", "abstract": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-04 BU data acquisition details." } }, { "ob_id": 11072, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24394, "uuid": "95be0404000143498d31efd99394dc23", "short_code": "acq", "title": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-25: data acquisition details", "abstract": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-25 data acquisition details." } }, { "ob_id": 11073, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24394, "uuid": "95be0404000143498d31efd99394dc23", "short_code": "acq", "title": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-25: data acquisition details", "abstract": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-25 data acquisition details." } }, { "ob_id": 11074, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24398, "uuid": "e53336a3d8474ce1b0e4b4ee8ffb36f1", "short_code": "acq", "title": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-26: data acquisition details", "abstract": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-26 data acquisition details." } }, { "ob_id": 11075, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24398, "uuid": "e53336a3d8474ce1b0e4b4ee8ffb36f1", "short_code": "acq", "title": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-26: data acquisition details", "abstract": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-26 data acquisition details." } }, { "ob_id": 11076, "platform": { "ob_id": 6389, "uuid": "23cc5b5b39a346cc80b98841da22d46e", "short_code": "plat", "title": "DO228-212 /D-CFFU - DLR aircraft", "abstract": "Medium tropospheric aircraft operated by Deutsches Zentrum fur Luft- und Raumfahrt e.V., Germany.\r\n\r\nThe Dornier 228 is a twin-turboprop STOL (short take-off and landing) utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier) from 1981 until 1998. This aircraft is part of the EUFAR fleet." }, "instrument": { "ob_id": 20354, "uuid": "add62b7ab00944999da4f0c973c858e8", "short_code": "instr", "title": "Airborne Prism Experiment (APEX)", "abstract": "The Airborne Prism Experiment (APEX) instrument is a hyperspectral remote sensing imaging spectrometer developed by a Swiss-Belgian consortium on behalf of ESA. It is being operated jointly by VITO Centre for Remote Sensing (Belgium) and RSL (Switzerland). http://www.apex-esa.org/. APEX is a dispersive pushbroom imaging spectrometer covering the solar reflected wavelength range between 372 and 2540 nm with nominal 312 (max. 532) spectral bands. APEX is calibrated using a combination of laboratory, in-flight and vicarious calibration approaches. These are complemented by using a forward and inverse radiative transfer modeling approach, suitable to further validate APEX data. It is flown on board the DLR dornier aircraft during EUFAR flights." }, "relatedTo": { "ob_id": 24402, "uuid": "4c221ba670c948d3be97683be891d4ca", "short_code": "acq", "title": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme2: data acquisition details", "abstract": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme2 data acquisition details." } }, { "ob_id": 11077, "platform": { "ob_id": 6389, "uuid": "23cc5b5b39a346cc80b98841da22d46e", "short_code": "plat", "title": "DO228-212 /D-CFFU - DLR aircraft", "abstract": "Medium tropospheric aircraft operated by Deutsches Zentrum fur Luft- und Raumfahrt e.V., Germany.\r\n\r\nThe Dornier 228 is a twin-turboprop STOL (short take-off and landing) utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier) from 1981 until 1998. This aircraft is part of the EUFAR fleet." }, "instrument": { "ob_id": 20354, "uuid": "add62b7ab00944999da4f0c973c858e8", "short_code": "instr", "title": "Airborne Prism Experiment (APEX)", "abstract": "The Airborne Prism Experiment (APEX) instrument is a hyperspectral remote sensing imaging spectrometer developed by a Swiss-Belgian consortium on behalf of ESA. It is being operated jointly by VITO Centre for Remote Sensing (Belgium) and RSL (Switzerland). http://www.apex-esa.org/. APEX is a dispersive pushbroom imaging spectrometer covering the solar reflected wavelength range between 372 and 2540 nm with nominal 312 (max. 532) spectral bands. APEX is calibrated using a combination of laboratory, in-flight and vicarious calibration approaches. These are complemented by using a forward and inverse radiative transfer modeling approach, suitable to further validate APEX data. It is flown on board the DLR dornier aircraft during EUFAR flights." }, "relatedTo": { "ob_id": 24407, "uuid": "7d6201a3d7474164a31e0348eb5d5fc2", "short_code": "acq", "title": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme1: data acquisition details", "abstract": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme1 data acquisition details." } }, { "ob_id": 11078, "platform": { "ob_id": 6389, "uuid": "23cc5b5b39a346cc80b98841da22d46e", "short_code": "plat", "title": "DO228-212 /D-CFFU - DLR aircraft", "abstract": "Medium tropospheric aircraft operated by Deutsches Zentrum fur Luft- und Raumfahrt e.V., Germany.\r\n\r\nThe Dornier 228 is a twin-turboprop STOL (short take-off and landing) utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier) from 1981 until 1998. This aircraft is part of the EUFAR fleet." }, "instrument": { "ob_id": 20354, "uuid": "add62b7ab00944999da4f0c973c858e8", "short_code": "instr", "title": "Airborne Prism Experiment (APEX)", "abstract": "The Airborne Prism Experiment (APEX) instrument is a hyperspectral remote sensing imaging spectrometer developed by a Swiss-Belgian consortium on behalf of ESA. It is being operated jointly by VITO Centre for Remote Sensing (Belgium) and RSL (Switzerland). http://www.apex-esa.org/. APEX is a dispersive pushbroom imaging spectrometer covering the solar reflected wavelength range between 372 and 2540 nm with nominal 312 (max. 532) spectral bands. APEX is calibrated using a combination of laboratory, in-flight and vicarious calibration approaches. These are complemented by using a forward and inverse radiative transfer modeling approach, suitable to further validate APEX data. It is flown on board the DLR dornier aircraft during EUFAR flights." }, "relatedTo": { "ob_id": 24411, "uuid": "95ad2e3fba3d4765a6fb17fa7965e68b", "short_code": "acq", "title": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme3: data acquisition details", "abstract": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme3 data acquisition details." } }, { "ob_id": 11079, "platform": { "ob_id": 6389, "uuid": "23cc5b5b39a346cc80b98841da22d46e", "short_code": "plat", "title": "DO228-212 /D-CFFU - DLR aircraft", "abstract": "Medium tropospheric aircraft operated by Deutsches Zentrum fur Luft- und Raumfahrt e.V., Germany.\r\n\r\nThe Dornier 228 is a twin-turboprop STOL (short take-off and landing) utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier) from 1981 until 1998. This aircraft is part of the EUFAR fleet." }, "instrument": { "ob_id": 20354, "uuid": "add62b7ab00944999da4f0c973c858e8", "short_code": "instr", "title": "Airborne Prism Experiment (APEX)", "abstract": "The Airborne Prism Experiment (APEX) instrument is a hyperspectral remote sensing imaging spectrometer developed by a Swiss-Belgian consortium on behalf of ESA. It is being operated jointly by VITO Centre for Remote Sensing (Belgium) and RSL (Switzerland). http://www.apex-esa.org/. APEX is a dispersive pushbroom imaging spectrometer covering the solar reflected wavelength range between 372 and 2540 nm with nominal 312 (max. 532) spectral bands. APEX is calibrated using a combination of laboratory, in-flight and vicarious calibration approaches. These are complemented by using a forward and inverse radiative transfer modeling approach, suitable to further validate APEX data. It is flown on board the DLR dornier aircraft during EUFAR flights." }, "relatedTo": { "ob_id": 24415, "uuid": "788e979c00ee47b8be084a15f39f5d29", "short_code": "acq", "title": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hymeb: data acquisition details", "abstract": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hymeb data acquisition details." } }, { "ob_id": 11080, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24419, "uuid": "6a7a9e45ce0e4588a2a43079169809de", "short_code": "acq", "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-06-30: data acquisition details", "abstract": "KIT-ENDURO EUFAR VESSAER Flight, 2012-06-30 data acquisition details." } }, { "ob_id": 11081, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24424, "uuid": "c0c4b79262c747acb50156fc54b1f472", "short_code": "acq", "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-01: data acquisition details", "abstract": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-01 data acquisition details." } }, { "ob_id": 11082, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24428, "uuid": "9cc4930c97674e0488df594298717b53", "short_code": "acq", "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-04: data acquisition details", "abstract": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-04 data acquisition details." } }, { "ob_id": 11083, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24432, "uuid": "285390cfe4654a05aa407a779f7a5608", "short_code": "acq", "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-06: data acquisition details", "abstract": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-06 data acquisition details." } }, { "ob_id": 11084, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24436, "uuid": "28094045de944a30aa4096fb033336ba", "short_code": "acq", "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-08: data acquisition details", "abstract": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-08 data acquisition details." } }, { "ob_id": 11085, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24440, "uuid": "8438dfb768d84b03be70847356ffb63f", "short_code": "acq", "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-09: data acquisition details", "abstract": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-09 data acquisition details." } }, { "ob_id": 11086, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24444, "uuid": "22e23ea37ab6494ca354b7cfa713140f", "short_code": "acq", "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-12: data acquisition details", "abstract": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-12 data acquisition details." } }, { "ob_id": 11087, "platform": { "ob_id": 6399, "uuid": "53ebb1bb71414347be1c2221894b2653", "short_code": "plat", "title": "ENDURO - KIT aircraft", "abstract": "The ENDURO model (Schmidtler, Munich, Germany) is a double-seated, flexible-wing, open-cockpit ultralight aircraft, maximum total weight at take off 400 kg, trike type. This ultralight aircraft is operated by Dr. Wolfgang Junkermann, Karlsruher Institut für Technologie, Germany.\r\n\r\nIt is powered by a ROTAX 582 two-stroke engine with 64 hp. The flexible wing (MILD, Air Creation, France) has an area of 16 m2. Total weight of the fueled aircraft is 240 kg, which provides, in addition to the pilot, a total of 90 kg payload, of which 45 kg are used for the currently installed instrumentation. A separate generator, independent from the aircraft generator, provides power for all instrumentation with a capacity of 200 W at 12 VDC.\r\nThis aircraft is part of the EUFAR TA fleet.\r\n\r\nOne of the main advantages of the open structure of ultralight aircraft is the very easy installation of instruments that can be rigidly attached to the mainframe tubes, often without the need of complicated air inlet systems. The push propeller enables the installation of all instruments in front of the engine and exhaust. All air inlets can be installed in undisturbed air in front of the aircraft and there is no need to cut holes into the aircraft shell." }, "instrument": { "ob_id": 20348, "uuid": "f959bf9b14dc4e4e8a42245a42345f07", "short_code": "instr", "title": "KIT Enduro core instruments", "abstract": "Instruments onboard the \tKIT Enduro aircraft operated by Karlsruhe Institute of Technology. May include: Incident flow vector probe, Optical Particle Counter (OPC), Nephelometer, Broad Band Radiometers (x3), Laser Altimeter, Black Carbon Aethelometer, Dew/Frost-point hygrometer, Inertial Reference/Navigation System, Ozone Analyzer, Condensation Particle Counter (CPC) plus others depending on the flight. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24448, "uuid": "7f8124f1de9f41f280657e945e9664c5", "short_code": "acq", "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-06-27: data acquisition details", "abstract": "KIT-ENDURO EUFAR VESSAER Flight, 2012-06-27 data acquisition details." } }, { "ob_id": 11088, "platform": { "ob_id": 11911, "uuid": "8291c6659fb04c0ead2af01941a79c0e", "short_code": "plat", "title": "ATR42 - SAFIRE aircraft", "abstract": "ATR42-SAFIRE is a large tropospheric research aircraft operated by Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe ATR 42 is a twin-turboprop, short-haul regional airliner built in France and Italy by ATR. The name \"42\" comes from the aircraft's standard seating, which varies from 40 to 52. The ATR-42 320 was designed to have better performance especially in hot and high conditions. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20344, "uuid": "9229a752355a4684b4a6c3b1dbdbe160", "short_code": "instr", "title": "SAFIRE ATR42 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-ATR42 aircraft. Includes Inertial Reference/Navigation System, Non dew/frost point hygrometer, Incident flow vector probe, Dew/Frost-point hygrometer, Global Positioning System, Broad Band Radiometer (x2), Temperature sensor (in situ) and Inertial Reference/Navigation System. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24452, "uuid": "1efedb43b3ef4b76b73f643f1b672cc9", "short_code": "acq", "title": "SAFIRE-ATR42 AS38 EUFAR WALITEMP Flight, 2012-09-13: data acquisition details", "abstract": "SAFIRE-ATR42 AS38 EUFAR WALITEMP Flight, 2012-09-13 data acquisition details." } }, { "ob_id": 11089, "platform": { "ob_id": 11911, "uuid": "8291c6659fb04c0ead2af01941a79c0e", "short_code": "plat", "title": "ATR42 - SAFIRE aircraft", "abstract": "ATR42-SAFIRE is a large tropospheric research aircraft operated by Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe ATR 42 is a twin-turboprop, short-haul regional airliner built in France and Italy by ATR. The name \"42\" comes from the aircraft's standard seating, which varies from 40 to 52. The ATR-42 320 was designed to have better performance especially in hot and high conditions. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20344, "uuid": "9229a752355a4684b4a6c3b1dbdbe160", "short_code": "instr", "title": "SAFIRE ATR42 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-ATR42 aircraft. Includes Inertial Reference/Navigation System, Non dew/frost point hygrometer, Incident flow vector probe, Dew/Frost-point hygrometer, Global Positioning System, Broad Band Radiometer (x2), Temperature sensor (in situ) and Inertial Reference/Navigation System. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24457, "uuid": "8c6b0d018a9d473facd7eac5c5c6a99c", "short_code": "acq", "title": "SAFIRE-ATR42 AS42 EUFAR WALITEMP Flight, 2012-10-02: data acquisition details", "abstract": "SAFIRE-ATR42 AS42 EUFAR WALITEMP Flight, 2012-10-02 data acquisition details." } }, { "ob_id": 11090, "platform": { "ob_id": 11911, "uuid": "8291c6659fb04c0ead2af01941a79c0e", "short_code": "plat", "title": "ATR42 - SAFIRE aircraft", "abstract": "ATR42-SAFIRE is a large tropospheric research aircraft operated by Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe ATR 42 is a twin-turboprop, short-haul regional airliner built in France and Italy by ATR. The name \"42\" comes from the aircraft's standard seating, which varies from 40 to 52. The ATR-42 320 was designed to have better performance especially in hot and high conditions. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20344, "uuid": "9229a752355a4684b4a6c3b1dbdbe160", "short_code": "instr", "title": "SAFIRE ATR42 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-ATR42 aircraft. Includes Inertial Reference/Navigation System, Non dew/frost point hygrometer, Incident flow vector probe, Dew/Frost-point hygrometer, Global Positioning System, Broad Band Radiometer (x2), Temperature sensor (in situ) and Inertial Reference/Navigation System. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24461, "uuid": "696723a5ce9443dfa7eb95b2020db82a", "short_code": "acq", "title": "SAFIRE-ATR42 AS57 EUFAR WALITEMP Flight, 2012-10-29: data acquisition details", "abstract": "SAFIRE-ATR42 AS57 EUFAR WALITEMP Flight, 2012-10-29 data acquisition details." } }, { "ob_id": 11091, "platform": { "ob_id": 11911, "uuid": "8291c6659fb04c0ead2af01941a79c0e", "short_code": "plat", "title": "ATR42 - SAFIRE aircraft", "abstract": "ATR42-SAFIRE is a large tropospheric research aircraft operated by Service des Avions Francais Instrumentés pour la Recherche en Environnement (SAFIRE), France.\r\nThe ATR 42 is a twin-turboprop, short-haul regional airliner built in France and Italy by ATR. The name \"42\" comes from the aircraft's standard seating, which varies from 40 to 52. The ATR-42 320 was designed to have better performance especially in hot and high conditions. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20344, "uuid": "9229a752355a4684b4a6c3b1dbdbe160", "short_code": "instr", "title": "SAFIRE ATR42 Core Instrument suite", "abstract": "SAFIRE (Service des Avions Francais Instrumentés pour la Recherche en Environnement) operated core instruments on board the SAFIRE-ATR42 aircraft. Includes Inertial Reference/Navigation System, Non dew/frost point hygrometer, Incident flow vector probe, Dew/Frost-point hygrometer, Global Positioning System, Broad Band Radiometer (x2), Temperature sensor (in situ) and Inertial Reference/Navigation System. Other optional instruments may be operated. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24465, "uuid": "94baec79f2e44b5b8f0cb9fcae1de03f", "short_code": "acq", "title": "SAFIRE-ATR42 AS62 EUFAR WALITEMP Flight, 2012-11-05: data acquisition details", "abstract": "SAFIRE-ATR42 AS62 EUFAR WALITEMP Flight, 2012-11-05 data acquisition details." } }, { "ob_id": 11092, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24469, "uuid": "716dca6d36634868b5ab88821be6959f", "short_code": "acq", "title": "INTACASA-RS EUFAR DEHESHYRE Flight, 2015-04-23: data acquisition details", "abstract": "INTACASA-RS EUFAR DEHESHYRE Flight, 2015-04-23 data acquisition details." } }, { "ob_id": 11093, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24469, "uuid": "716dca6d36634868b5ab88821be6959f", "short_code": "acq", "title": "INTACASA-RS EUFAR DEHESHYRE Flight, 2015-04-23: data acquisition details", "abstract": "INTACASA-RS EUFAR DEHESHYRE Flight, 2015-04-23 data acquisition details." } }, { "ob_id": 11094, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24474, "uuid": "8903f999aac94b158a9e98300c7aeb41", "short_code": "acq", "title": "INTACASA-RS EUFAR DEHESHYRE Flight, 2015-07-03: data acquisition details", "abstract": "INTACASA-RS EUFAR DEHESHYRE Flight, 2015-07-03 data acquisition details." } }, { "ob_id": 11095, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24474, "uuid": "8903f999aac94b158a9e98300c7aeb41", "short_code": "acq", "title": "INTACASA-RS EUFAR DEHESHYRE Flight, 2015-07-03: data acquisition details", "abstract": "INTACASA-RS EUFAR DEHESHYRE Flight, 2015-07-03 data acquisition details." } }, { "ob_id": 11096, "platform": { "ob_id": 6389, "uuid": "23cc5b5b39a346cc80b98841da22d46e", "short_code": "plat", "title": "DO228-212 /D-CFFU - DLR aircraft", "abstract": "Medium tropospheric aircraft operated by Deutsches Zentrum fur Luft- und Raumfahrt e.V., Germany.\r\n\r\nThe Dornier 228 is a twin-turboprop STOL (short take-off and landing) utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier) from 1981 until 1998. This aircraft is part of the EUFAR fleet." }, "instrument": { "ob_id": 20354, "uuid": "add62b7ab00944999da4f0c973c858e8", "short_code": "instr", "title": "Airborne Prism Experiment (APEX)", "abstract": "The Airborne Prism Experiment (APEX) instrument is a hyperspectral remote sensing imaging spectrometer developed by a Swiss-Belgian consortium on behalf of ESA. It is being operated jointly by VITO Centre for Remote Sensing (Belgium) and RSL (Switzerland). http://www.apex-esa.org/. APEX is a dispersive pushbroom imaging spectrometer covering the solar reflected wavelength range between 372 and 2540 nm with nominal 312 (max. 532) spectral bands. APEX is calibrated using a combination of laboratory, in-flight and vicarious calibration approaches. These are complemented by using a forward and inverse radiative transfer modeling approach, suitable to further validate APEX data. It is flown on board the DLR dornier aircraft during EUFAR flights." }, "relatedTo": { "ob_id": 24478, "uuid": "efd30e55a9ac487f84e80fd7f7f4be2d", "short_code": "acq", "title": "APEX EUFAR HILBILLY Flight, 2015-07-10 LakeBiel: data acquisition details", "abstract": "APEX EUFAR HILBILLY Flight, 2015-07-10 LakeBiel data acquisition details." } }, { "ob_id": 11097, "platform": { "ob_id": 6389, "uuid": "23cc5b5b39a346cc80b98841da22d46e", "short_code": "plat", "title": "DO228-212 /D-CFFU - DLR aircraft", "abstract": "Medium tropospheric aircraft operated by Deutsches Zentrum fur Luft- und Raumfahrt e.V., Germany.\r\n\r\nThe Dornier 228 is a twin-turboprop STOL (short take-off and landing) utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier) from 1981 until 1998. This aircraft is part of the EUFAR fleet." }, "instrument": { "ob_id": 20354, "uuid": "add62b7ab00944999da4f0c973c858e8", "short_code": "instr", "title": "Airborne Prism Experiment (APEX)", "abstract": "The Airborne Prism Experiment (APEX) instrument is a hyperspectral remote sensing imaging spectrometer developed by a Swiss-Belgian consortium on behalf of ESA. It is being operated jointly by VITO Centre for Remote Sensing (Belgium) and RSL (Switzerland). http://www.apex-esa.org/. APEX is a dispersive pushbroom imaging spectrometer covering the solar reflected wavelength range between 372 and 2540 nm with nominal 312 (max. 532) spectral bands. APEX is calibrated using a combination of laboratory, in-flight and vicarious calibration approaches. These are complemented by using a forward and inverse radiative transfer modeling approach, suitable to further validate APEX data. It is flown on board the DLR dornier aircraft during EUFAR flights." }, "relatedTo": { "ob_id": 24483, "uuid": "f3fdf2176f9e4939b7e35eb3b1474c86", "short_code": "acq", "title": "APEX EUFAR HILBILLY Flight, 2015-07-10 LakeGeneve: data acquisition details", "abstract": "APEX EUFAR HILBILLY Flight, 2015-07-10 LakeGeneve data acquisition details." } }, { "ob_id": 11098, "platform": { "ob_id": 6389, "uuid": "23cc5b5b39a346cc80b98841da22d46e", "short_code": "plat", "title": "DO228-212 /D-CFFU - DLR aircraft", "abstract": "Medium tropospheric aircraft operated by Deutsches Zentrum fur Luft- und Raumfahrt e.V., Germany.\r\n\r\nThe Dornier 228 is a twin-turboprop STOL (short take-off and landing) utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier) from 1981 until 1998. This aircraft is part of the EUFAR fleet." }, "instrument": { "ob_id": 20354, "uuid": "add62b7ab00944999da4f0c973c858e8", "short_code": "instr", "title": "Airborne Prism Experiment (APEX)", "abstract": "The Airborne Prism Experiment (APEX) instrument is a hyperspectral remote sensing imaging spectrometer developed by a Swiss-Belgian consortium on behalf of ESA. It is being operated jointly by VITO Centre for Remote Sensing (Belgium) and RSL (Switzerland). http://www.apex-esa.org/. APEX is a dispersive pushbroom imaging spectrometer covering the solar reflected wavelength range between 372 and 2540 nm with nominal 312 (max. 532) spectral bands. APEX is calibrated using a combination of laboratory, in-flight and vicarious calibration approaches. These are complemented by using a forward and inverse radiative transfer modeling approach, suitable to further validate APEX data. It is flown on board the DLR dornier aircraft during EUFAR flights." }, "relatedTo": { "ob_id": 24487, "uuid": "2ef5e9633c864d33b35d7bdf68765d9f", "short_code": "acq", "title": "APEX EUFAR HILBILLY Flight, 2015-07-11 LakeGeneve: data acquisition details", "abstract": "APEX EUFAR HILBILLY Flight, 2015-07-11 LakeGeneve data acquisition details." } }, { "ob_id": 11099, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24491, "uuid": "c0d2e8d2fe7742529bdae22b1d6cc9d4", "short_code": "acq", "title": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Leuven: data acquisition details", "abstract": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Leuven data acquisition details." } }, { "ob_id": 11100, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24491, "uuid": "c0d2e8d2fe7742529bdae22b1d6cc9d4", "short_code": "acq", "title": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Leuven: data acquisition details", "abstract": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Leuven data acquisition details." } }, { "ob_id": 11101, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24496, "uuid": "11095ea84117415e88d0d091b0b68d85", "short_code": "acq", "title": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Ghent: data acquisition details", "abstract": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Ghent data acquisition details." } }, { "ob_id": 11102, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24496, "uuid": "11095ea84117415e88d0d091b0b68d85", "short_code": "acq", "title": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Ghent: data acquisition details", "abstract": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Ghent data acquisition details." } }, { "ob_id": 11103, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20342, "uuid": "f683fac83ae24d8e9fda96e0e49d50e3", "short_code": "instr", "title": "INTA Airborne Hyperspectral Scanner", "abstract": "Argonst Airborne Hyperspectral Scanner measures Radiance Spectra. Operated on the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24500, "uuid": "908a3acabeac4ddcb07930d595b1e62a", "short_code": "acq", "title": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Brussels: data acquisition details", "abstract": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Brussels data acquisition details." } }, { "ob_id": 11104, "platform": { "ob_id": 6397, "uuid": "037858ab9726427e84907eb282137ac4", "short_code": "plat", "title": "CASA 212 RS - INTA aircraft", "abstract": "CASA 212 RS - INTA is a medium tropospheric aircraft operated by Instituto Nacional de Tecnica Aeroespacial, Spain. This is a twin-engine turboprop-powered STOL medium transport aircraft designed and built in Spain. This aircraft is part of the EUFAR TA fleet" }, "instrument": { "ob_id": 20343, "uuid": "0dc7ea5d95ed4d63a220d9d145b82a1c", "short_code": "instr", "title": "INTA Compact Airborne Spectrographic Imager 1500i", "abstract": "INTA Compact Airborne Spectrographic Imager 1500i is an Imaging Spectrometer operated on board the INTA-CASA-RS aircraft. Used in EUFAR flights." }, "relatedTo": { "ob_id": 24500, "uuid": "908a3acabeac4ddcb07930d595b1e62a", "short_code": "acq", "title": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Brussels: data acquisition details", "abstract": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Brussels data acquisition details." } } ] }