Mobile Platform Operation List

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            "short_code": "mpop",
            "title": "APEX EUFAR HYPERSTRESS Flight, 2011-09-08: flight details over Valencia area, eastern Spain",
            "abstract": "Flight details for APEX EUFAR HYPERSTRESS Flight, 2011-09-08 over Valencia area, eastern Spain. See linked documentation for further details.",
            "status": "completed",
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                "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."
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                "startTime": "2011-09-08T11:00:00",
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            "short_code": "mpop",
            "title": "INTACASA-RS EUFAR IMROM Flight, 2011-07-25: flight details over Rosia Montana, west-central Romania",
            "abstract": "Flight details for INTACASA-RS EUFAR IMROM Flight, 2011-07-25 over Rosia Montana, west-central Romania. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
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                "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"
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                "startTime": "2011-07-25T07:29:00",
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            "uuid": "b54eb10050b2485683cdfd86a53c9c61",
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            "title": "APEX EUFAR HYPPOS Flight, 2014-09-27: flight details over Mantua, Northern Italy",
            "abstract": "Flight details for APEX EUFAR HYPPOS Flight, 2014-09-27 over Mantua, Northern Italy. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
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                "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."
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                "startTime": "2014-09-27T11:00:00",
                "endTime": "2014-09-27T11:30:00"
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            "short_code": "mpop",
            "title": "SAFIRE-FA20 FS13 EUFAR RAIN4DUST Flight, 2011-06-11: flight details over Central Saharan mountains, Chad",
            "abstract": "Flight details for SAFIRE-FA20 FS13 EUFAR RAIN4DUST Flight, 2011-06-11 over Central Saharan mountains, Chad. See linked documentation for further details.",
            "status": "completed",
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                "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."
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                "startTime": "2011-06-11T07:47:39",
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            "short_code": "mpop",
            "title": "SAFIRE-FA20 FS18 EUFAR RAIN4DUST Flight, 2011-06-16: flight details over Central Saharan mountains, Chad",
            "abstract": "Flight details for SAFIRE-FA20 FS18 EUFAR RAIN4DUST Flight, 2011-06-16 over Central Saharan mountains, Chad. See linked documentation for further details.",
            "status": "completed",
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                "uuid": "32ce062fe89a4c1eb8ab3e67c1f9ad45",
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                "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."
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            "short_code": "mpop",
            "title": "SAFIRE-FA20 FS26 EUFAR RAIN4DUST Flight, 2011-06-23: flight details over Central Saharan mountains, Chad",
            "abstract": "Flight details for SAFIRE-FA20 FS26 EUFAR RAIN4DUST Flight, 2011-06-23 over Central Saharan mountains, Chad. See linked documentation for further details.",
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                "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."
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                "startTime": "2011-06-23T07:25:08",
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            "short_code": "mpop",
            "title": "INTACASA-RS EUFAR UR-TIR Flight, 2011-07-05: flight details over Munich and Bochum, Germany",
            "abstract": "Flight details for INTACASA-RS EUFAR UR-TIR Flight, 2011-07-05 over Munich and Bochum, Germany. See linked documentation for further details.",
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                "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"
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                "startTime": "2011-07-05T10:10:00",
                "endTime": "2011-07-05T10:19:00"
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            "short_code": "mpop",
            "title": "INTACASA-RS EUFAR UR-TIR Flight, 2011-07-12: flight details over Munich and Bochum, Germany",
            "abstract": "Flight details for INTACASA-RS EUFAR UR-TIR Flight, 2011-07-12 over Munich and Bochum, Germany. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
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                "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"
            },
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                "startTime": "2011-07-11T23:00:00",
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            "short_code": "mpop",
            "title": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-04 BU: flight details over Albacete, Spain",
            "abstract": "Flight details for INTACASA-RS EUFAR REFLEX Flight, 2012-07-04 BU over Albacete, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
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                "startTime": "2012-07-04T09:17:00",
                "endTime": "2012-07-04T09:18:00"
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            "short_code": "mpop",
            "title": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-25: flight details over Albacete, Spain",
            "abstract": "Flight details for INTACASA-RS EUFAR REFLEX Flight, 2012-07-25 over Albacete, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
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                "ob_id": 6628,
                "startTime": "2012-07-25T21:40:00",
                "endTime": "2012-07-25T21:40:00"
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            "short_code": "mpop",
            "title": "INTACASA-RS EUFAR REFLEX Flight, 2012-07-26: flight details over Albacete, Spain",
            "abstract": "Flight details for INTACASA-RS EUFAR REFLEX Flight, 2012-07-26 over Albacete, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
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            "operationTime": {
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                "startTime": "2012-07-25T23:00:00",
                "endTime": "2012-07-26T22:59:59"
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            "short_code": "mpop",
            "title": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme2: flight details over Giant Mountains (Karkonosze/Krkonose) National Park.  Border of the Czech Republic and Poland",
            "abstract": "Flight details for APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme2 over Giant Mountains (Karkonosze/Krkonose) National Park.  Border of the Czech Republic and Poland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
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                "startTime": "2012-09-10T11:00:00",
                "endTime": "2012-09-10T11:30:00"
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            "short_code": "mpop",
            "title": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme1: flight details over Giant Mountains (Karkonosze/Krkonose) National Park.  Border of the Czech Republic and Poland",
            "abstract": "Flight details for APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme1 over Giant Mountains (Karkonosze/Krkonose) National Park.  Border of the Czech Republic and Poland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
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                "startTime": "2012-09-10T11:00:00",
                "endTime": "2012-09-10T11:30:00"
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            "short_code": "mpop",
            "title": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme3: flight details over Giant Mountains (Karkonosze/Krkonose) National Park.  Border of the Czech Republic and Poland",
            "abstract": "Flight details for APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hyme3 over Giant Mountains (Karkonosze/Krkonose) National Park.  Border of the Czech Republic and Poland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
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                "ob_id": 6632,
                "startTime": "2012-09-10T11:00:00",
                "endTime": "2012-09-10T11:30:00"
            },
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            "uuid": "9ad75cda251941488a5d59d3dde9ecc9",
            "short_code": "mpop",
            "title": "APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hymeb: flight details over Giant Mountains (Karkonosze/Krkonose) National Park.  Border of the Czech Republic and Poland",
            "abstract": "Flight details for APEX EUFAR HYMOUNTECOS Flight, 2012-09-10 hymeb over Giant Mountains (Karkonosze/Krkonose) National Park.  Border of the Czech Republic and Poland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6633,
                "startTime": "2012-09-10T11:00:00",
                "endTime": "2012-09-10T11:30:00"
            },
            "childOperation": null
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            "short_code": "mpop",
            "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-06-30: flight details over Corsica, France",
            "abstract": "Flight details for KIT-ENDURO EUFAR VESSAER Flight, 2012-06-30 over Corsica, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6634,
                "startTime": "2012-06-30T06:28:35",
                "endTime": "2012-06-30T09:17:28"
            },
            "childOperation": null
        },
        {
            "ob_id": 24425,
            "uuid": "ce068d6be627487f90ca00702a9b13b8",
            "short_code": "mpop",
            "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-01: flight details over Corsica, France",
            "abstract": "Flight details for KIT-ENDURO EUFAR VESSAER Flight, 2012-07-01 over Corsica, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6635,
                "startTime": "2012-06-30T23:00:00",
                "endTime": "2012-07-01T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24429,
            "uuid": "a03bd98d8a67430ab148d114c8993b86",
            "short_code": "mpop",
            "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-04: flight details over Corsica, France",
            "abstract": "Flight details for KIT-ENDURO EUFAR VESSAER Flight, 2012-07-04 over Corsica, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6636,
                "startTime": "2012-07-03T23:00:00",
                "endTime": "2012-07-04T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24433,
            "uuid": "43cfd27f102042c69cdf29422e342809",
            "short_code": "mpop",
            "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-06: flight details over Corsica, France",
            "abstract": "Flight details for KIT-ENDURO EUFAR VESSAER Flight, 2012-07-06 over Corsica, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6637,
                "startTime": "2012-07-05T23:00:00",
                "endTime": "2012-07-06T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24437,
            "uuid": "a76bb703987744fbb8e7b4a91ca968d2",
            "short_code": "mpop",
            "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-08: flight details over Corsica, France",
            "abstract": "Flight details for KIT-ENDURO EUFAR VESSAER Flight, 2012-07-08 over Corsica, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6638,
                "startTime": "2012-07-07T23:00:00",
                "endTime": "2012-07-08T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24441,
            "uuid": "294f4ba834094ade8dee9d622e5ad845",
            "short_code": "mpop",
            "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-09: flight details over Corsica, France",
            "abstract": "Flight details for KIT-ENDURO EUFAR VESSAER Flight, 2012-07-09 over Corsica, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6639,
                "startTime": "2012-07-08T23:00:00",
                "endTime": "2012-07-09T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24445,
            "uuid": "0b4c2328b1e647f3ac744fa12190b4e1",
            "short_code": "mpop",
            "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-07-12: flight details over Corsica, France",
            "abstract": "Flight details for KIT-ENDURO EUFAR VESSAER Flight, 2012-07-12 over Corsica, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6640,
                "startTime": "2012-07-11T23:00:00",
                "endTime": "2012-07-12T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24449,
            "uuid": "9184593059634fd5a1fbb3228ea46c5d",
            "short_code": "mpop",
            "title": "KIT-ENDURO EUFAR VESSAER Flight, 2012-06-27: flight details over Corsica, France",
            "abstract": "Flight details for KIT-ENDURO EUFAR VESSAER Flight, 2012-06-27 over Corsica, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6641,
                "startTime": "2012-06-30T06:28:35",
                "endTime": "2012-06-30T09:17:28"
            },
            "childOperation": null
        },
        {
            "ob_id": 24453,
            "uuid": "e147b241a4954ce2b8bff1489f279012",
            "short_code": "mpop",
            "title": "SAFIRE-ATR42 AS38 EUFAR WALITEMP Flight, 2012-09-13: flight details over Montpellier, France. Mediterranean Basin",
            "abstract": "Flight details for SAFIRE-ATR42 AS38 EUFAR WALITEMP Flight, 2012-09-13 over Montpellier, France. Mediterranean Basin. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
            "location": {
                "ob_id": 1736,
                "bboxName": "",
                "eastBoundLongitude": 4.339716911315918,
                "westBoundLongitude": 3.9490134716033936,
                "southBoundLatitude": 43.46342849731445,
                "northBoundLatitude": 43.70265579223633
            },
            "operationTime": {
                "ob_id": 6642,
                "startTime": "2012-09-13T17:50:47",
                "endTime": "2012-09-13T19:49:54"
            },
            "childOperation": null
        },
        {
            "ob_id": 24458,
            "uuid": "2a542e64a6be4f3ca02d8bf51cb9977e",
            "short_code": "mpop",
            "title": "SAFIRE-ATR42 AS42 EUFAR WALITEMP Flight, 2012-10-02: flight details over Montpellier, France. Mediterranean Basin",
            "abstract": "Flight details for SAFIRE-ATR42 AS42 EUFAR WALITEMP Flight, 2012-10-02 over Montpellier, France. Mediterranean Basin. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
            "location": {
                "ob_id": 1737,
                "bboxName": "",
                "eastBoundLongitude": 4.350677013397217,
                "westBoundLongitude": 3.953430414199829,
                "southBoundLatitude": 43.53447723388672,
                "northBoundLatitude": 43.74720001220703
            },
            "operationTime": {
                "ob_id": 6643,
                "startTime": "2012-10-02T18:00:08",
                "endTime": "2012-10-02T21:13:12"
            },
            "childOperation": null
        },
        {
            "ob_id": 24462,
            "uuid": "afe45c0750d24cb8b7c9b5884d7ba711",
            "short_code": "mpop",
            "title": "SAFIRE-ATR42 AS57 EUFAR WALITEMP Flight, 2012-10-29: flight details over Montpellier, France. Mediterranean Basin",
            "abstract": "Flight details for SAFIRE-ATR42 AS57 EUFAR WALITEMP Flight, 2012-10-29 over Montpellier, France. Mediterranean Basin. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
            "location": {
                "ob_id": 1738,
                "bboxName": "",
                "eastBoundLongitude": 4.370481967926025,
                "westBoundLongitude": 3.9438233375549316,
                "southBoundLatitude": 43.44947052001953,
                "northBoundLatitude": 43.70111083984375
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            "operationTime": {
                "ob_id": 6644,
                "startTime": "2012-10-29T13:20:41",
                "endTime": "2012-10-29T16:39:54"
            },
            "childOperation": null
        },
        {
            "ob_id": 24466,
            "uuid": "c4c9b7469c5b4658bfae70c6363d77c2",
            "short_code": "mpop",
            "title": "SAFIRE-ATR42 AS62 EUFAR WALITEMP Flight, 2012-11-05: flight details over Montpellier, France. Mediterranean Basin",
            "abstract": "Flight details for SAFIRE-ATR42 AS62 EUFAR WALITEMP Flight, 2012-11-05 over Montpellier, France. Mediterranean Basin. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
            "location": {
                "ob_id": 1739,
                "bboxName": "",
                "eastBoundLongitude": 4.33854866027832,
                "westBoundLongitude": 3.953489303588867,
                "southBoundLatitude": 43.56466293334961,
                "northBoundLatitude": 43.678680419921875
            },
            "operationTime": {
                "ob_id": 6645,
                "startTime": "2012-11-05T09:28:42",
                "endTime": "2012-11-05T12:38:36"
            },
            "childOperation": null
        },
        {
            "ob_id": 24470,
            "uuid": "2adac98e47034153bb0f02a874b3d3c3",
            "short_code": "mpop",
            "title": "INTACASA-RS EUFAR DEHESHYRE Flight, 2015-04-23: flight details over Las Majadas del Tieta, Spain",
            "abstract": "Flight details for INTACASA-RS EUFAR DEHESHYRE Flight, 2015-04-23 over Las Majadas del Tieta, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6646,
                "startTime": "2015-04-23T10:37:00",
                "endTime": "2015-04-23T10:38:00"
            },
            "childOperation": null
        },
        {
            "ob_id": 24475,
            "uuid": "aa49ff5609194d0db6b04ea2a797f2b8",
            "short_code": "mpop",
            "title": "INTACASA-RS EUFAR DEHESHYRE Flight, 2015-07-03: flight details over Las Majadas del Tieta, Spain",
            "abstract": "Flight details for INTACASA-RS EUFAR DEHESHYRE Flight, 2015-07-03 over Las Majadas del Tieta, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6647,
                "startTime": "2015-07-02T23:00:00",
                "endTime": "2015-07-03T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24479,
            "uuid": "d0a5bcb1fe7049a697c480bf8e0938e8",
            "short_code": "mpop",
            "title": "APEX EUFAR HILBILLY Flight, 2015-07-10 LakeBiel: flight details over Lake Biel and Lake Geneva, Switzerland",
            "abstract": "Flight details for APEX EUFAR HILBILLY Flight, 2015-07-10 LakeBiel over Lake Biel and Lake Geneva, Switzerland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6648,
                "startTime": "2015-07-10T11:00:00",
                "endTime": "2015-07-10T11:30:00"
            },
            "childOperation": null
        },
        {
            "ob_id": 24484,
            "uuid": "3a34d2e935e24374b4537d1c2e383856",
            "short_code": "mpop",
            "title": "APEX EUFAR HILBILLY Flight, 2015-07-10 LakeGeneve: flight details over Lake Biel and Lake Geneva, Switzerland",
            "abstract": "Flight details for APEX EUFAR HILBILLY Flight, 2015-07-10 LakeGeneve over Lake Biel and Lake Geneva, Switzerland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6649,
                "startTime": "2015-07-10T11:00:00",
                "endTime": "2015-07-10T11:30:00"
            },
            "childOperation": null
        },
        {
            "ob_id": 24488,
            "uuid": "7c93df59621448b096f82eb0aa003656",
            "short_code": "mpop",
            "title": "APEX EUFAR HILBILLY Flight, 2015-07-11 LakeGeneve: flight details over Lake Biel and Lake Geneva, Switzerland",
            "abstract": "Flight details for APEX EUFAR HILBILLY Flight, 2015-07-11 LakeGeneve over Lake Biel and Lake Geneva, Switzerland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6650,
                "startTime": "2015-07-10T23:00:00",
                "endTime": "2015-07-11T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24492,
            "uuid": "4e94a477b2204a6f900c4b6e0e279caa",
            "short_code": "mpop",
            "title": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Leuven: flight details over Brussels, Ghent, Leuven, Belgium",
            "abstract": "Flight details for INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Leuven over Brussels, Ghent, Leuven, Belgium. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6651,
                "startTime": "2015-07-10T11:22:00",
                "endTime": "2015-07-10T11:26:00"
            },
            "childOperation": null
        },
        {
            "ob_id": 24497,
            "uuid": "9c7276689f2043d586e02992dafe4754",
            "short_code": "mpop",
            "title": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Ghent: flight details over Brussels, Ghent, Leuven, Belgium",
            "abstract": "Flight details for INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Ghent over Brussels, Ghent, Leuven, Belgium. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6652,
                "startTime": "2015-07-10T11:52:00",
                "endTime": "2015-07-10T11:56:00"
            },
            "childOperation": null
        },
        {
            "ob_id": 24501,
            "uuid": "a374924115954e87ac5758d60342dc2a",
            "short_code": "mpop",
            "title": "INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Brussels: flight details over Brussels, Ghent, Leuven, Belgium",
            "abstract": "Flight details for INTACASA-RS EUFAR URBSENSE Flight, 2015-07-10 Brussels over Brussels, Ghent, Leuven, Belgium. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6653,
                "startTime": "2015-07-10T09:43:00",
                "endTime": "2015-07-10T09:47:00"
            },
            "childOperation": null
        },
        {
            "ob_id": 24505,
            "uuid": "dc8e4b3563ca4b3a93be56c42ecd77f3",
            "short_code": "mpop",
            "title": "APEX EUFAR SWAMP Flight, 2015-07-15: flight details over Rzecin peatland site (PolWet) Site, western Poland",
            "abstract": "Flight details for APEX EUFAR SWAMP Flight, 2015-07-15 over Rzecin peatland site (PolWet) Site, western Poland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6654,
                "startTime": "2015-07-15T11:00:00",
                "endTime": "2015-07-15T11:30:00"
            },
            "childOperation": null
        },
        {
            "ob_id": 24510,
            "uuid": "e6b03cf50da34d7baf2798b0ff2b23ae",
            "short_code": "mpop",
            "title": "APEX EUFAR AROMAPEX Flight, 2016-04-21 M0152-Berlin-AM: flight details over Berlin, Germany",
            "abstract": "Flight details for APEX EUFAR AROMAPEX Flight, 2016-04-21 M0152-Berlin-AM over Berlin, Germany. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6655,
                "startTime": "2016-04-21T11:00:00",
                "endTime": "2016-04-21T11:30:00"
            },
            "childOperation": null
        },
        {
            "ob_id": 24515,
            "uuid": "5e8f9cbf104a475f8f18430fe0ea6224",
            "short_code": "mpop",
            "title": "APEX EUFAR AROMAPEX Flight, 2016-04-21 M0153-Berlin-PM: flight details over Berlin, Germany",
            "abstract": "Flight details for APEX EUFAR AROMAPEX Flight, 2016-04-21 M0153-Berlin-PM over Berlin, Germany. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "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."
            },
            "location": null,
            "operationTime": {
                "ob_id": 6656,
                "startTime": "2016-04-21T11:00:00",
                "endTime": "2016-04-21T11:30:00"
            },
            "childOperation": null
        },
        {
            "ob_id": 24519,
            "uuid": "a887ff96367744038cfd27d7077bf2a4",
            "short_code": "mpop",
            "title": "ARSF 2010_233b - EUFAR AIMWETLAB/EUFAR10_01 Flight: flight details over Balaton Peninsula, Hungary",
            "abstract": "Flight details for ARSF 2010_233b - EUFAR AIMWETLAB/EUFAR10_01 Flight over Balaton Peninsula, Hungary. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6657,
                "startTime": "2010-08-20T23:00:00",
                "endTime": "2010-08-21T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24524,
            "uuid": "2bd7b66f5d0c45fc99b873db81a1ca03",
            "short_code": "mpop",
            "title": "ARSF 2010_234e - EUFAR AIMWETLAB/EUFAR10_01 Flight: flight details over Balaton Peninsula, Hungary",
            "abstract": "Flight details for ARSF 2010_234e - EUFAR AIMWETLAB/EUFAR10_01 Flight over Balaton Peninsula, Hungary. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6658,
                "startTime": "2010-08-21T23:00:00",
                "endTime": "2010-08-22T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24528,
            "uuid": "c0d04d07c9554b2db33aa30921ec17ad",
            "short_code": "mpop",
            "title": "ARSF 2010_235b - EUFAR AIMWETLAB/EUFAR10_01 Flight: flight details over Balaton Peninsula, Hungary",
            "abstract": "Flight details for ARSF 2010_235b - EUFAR AIMWETLAB/EUFAR10_01 Flight over Balaton Peninsula, Hungary. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6659,
                "startTime": "2010-08-22T23:00:00",
                "endTime": "2010-08-23T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24532,
            "uuid": "1b698fa0ed63496bb5cd97b056f59cf8",
            "short_code": "mpop",
            "title": "ARSF 2010_238b - EUFAR AIMWETLAB/EUFAR10_01 Flight: flight details over Balaton Peninsula, Hungary",
            "abstract": "Flight details for ARSF 2010_238b - EUFAR AIMWETLAB/EUFAR10_01 Flight over Balaton Peninsula, Hungary. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6660,
                "startTime": "2010-08-25T23:00:00",
                "endTime": "2010-08-26T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24536,
            "uuid": "6f3dc1f22b3840b79b91b19740d1d9a6",
            "short_code": "mpop",
            "title": "ARSF 2010_199a - EUFAR AIRES-CZM/EUFAR10_02 Flight: flight details over Santander, Spain",
            "abstract": "Flight details for ARSF 2010_199a - EUFAR AIRES-CZM/EUFAR10_02 Flight over Santander, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6661,
                "startTime": "2010-07-17T23:00:00",
                "endTime": "2010-07-18T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24541,
            "uuid": "73a546b7fa2d4fd191e023a177175cdc",
            "short_code": "mpop",
            "title": "ARSF 2010_199b - EUFAR AIRES-CZM/EUFAR10_02 Flight: flight details over Santander, Spain",
            "abstract": "Flight details for ARSF 2010_199b - EUFAR AIRES-CZM/EUFAR10_02 Flight over Santander, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6662,
                "startTime": "2010-07-17T23:00:00",
                "endTime": "2010-07-18T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24545,
            "uuid": "9fac5f10061e44bfa7caed8dbed22897",
            "short_code": "mpop",
            "title": "ARSF 2010_200 - EUFAR AIRES-CZM/EUFAR10_02 Flight: flight details over Santander, Spain",
            "abstract": "Flight details for ARSF 2010_200 - EUFAR AIRES-CZM/EUFAR10_02 Flight over Santander, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6663,
                "startTime": "2010-07-18T23:00:00",
                "endTime": "2010-07-19T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24549,
            "uuid": "bd08e7e020c74966bdf087ed06fbbc05",
            "short_code": "mpop",
            "title": "ARSF 2010_231a - EUFAR ARMSRACE/EUFAR10_06 Flight: flight details over Sarviz Valley, Hungary",
            "abstract": "Flight details for ARSF 2010_231a - EUFAR ARMSRACE/EUFAR10_06 Flight over Sarviz Valley, Hungary. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6664,
                "startTime": "2010-08-18T23:00:00",
                "endTime": "2010-08-19T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24554,
            "uuid": "863449dae84b451986e45c051bf40aab",
            "short_code": "mpop",
            "title": "ARSF 2010_196 - EUFAR A-NEW/EUFAR10_03 Flight: flight details over Lisbon, Portugal",
            "abstract": "Flight details for ARSF 2010_196 - EUFAR A-NEW/EUFAR10_03 Flight over Lisbon, Portugal. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6665,
                "startTime": "2010-07-14T23:00:00",
                "endTime": "2010-07-15T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24559,
            "uuid": "2d2207ed0a334c9eb22fd9b2d7e36273",
            "short_code": "mpop",
            "title": "ARSF 2010_197 - EUFAR A-NEW/EUFAR10_03 Flight: flight details over Lisbon, Portugal",
            "abstract": "Flight details for ARSF 2010_197 - EUFAR A-NEW/EUFAR10_03 Flight over Lisbon, Portugal. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6666,
                "startTime": "2010-07-15T23:00:00",
                "endTime": "2010-07-16T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24563,
            "uuid": "edf945f54a0a4ab49c41fb95fd9dc68f",
            "short_code": "mpop",
            "title": "ARSF 2010_234b - EUFAR ADDRESSS/EUFAR10_07 Flight: flight details over Tihany, Hungary",
            "abstract": "Flight details for ARSF 2010_234b - EUFAR ADDRESSS/EUFAR10_07 Flight over Tihany, Hungary. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6667,
                "startTime": "2010-08-21T23:00:00",
                "endTime": "2010-08-22T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24568,
            "uuid": "7250413211574566b71dd006483ff355",
            "short_code": "mpop",
            "title": "ARSF 2010_234d - EUFAR ADDRESSS/EUFAR10_07 Flight: flight details over Tihany, Hungary",
            "abstract": "Flight details for ARSF 2010_234d - EUFAR ADDRESSS/EUFAR10_07 Flight over Tihany, Hungary. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6668,
                "startTime": "2010-08-21T23:00:00",
                "endTime": "2010-08-22T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24572,
            "uuid": "3df47094cd014a1185d953704e2ac885",
            "short_code": "mpop",
            "title": "ARSF 2010_301 - EUFAR VALCALHYP/EUFAR10_08 Flight: flight details over Toulouse, France",
            "abstract": "Flight details for ARSF 2010_301 - EUFAR VALCALHYP/EUFAR10_08 Flight over Toulouse, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6669,
                "startTime": "2010-10-27T23:00:00",
                "endTime": "2010-10-28T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24576,
            "uuid": "842106fddb05473b9eaba1c95ca8959d",
            "short_code": "mpop",
            "title": "ARSF 2011_092 - EUFAR HYMEDECOS-EROSION/EUFAR11_03 Flight: flight details over North East Spain",
            "abstract": "Flight details for ARSF 2011_092 - EUFAR HYMEDECOS-EROSION/EUFAR11_03 Flight over North East Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6670,
                "startTime": "2011-04-01T23:00:00",
                "endTime": "2011-04-02T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24581,
            "uuid": "f93894b936a84ec2866c68745ce4e91f",
            "short_code": "mpop",
            "title": "ARSF 2011_095 - EUFAR HYMEDECOS-EROSION/EUFAR11_03 Flight: flight details over North East Spain",
            "abstract": "Flight details for ARSF 2011_095 - EUFAR HYMEDECOS-EROSION/EUFAR11_03 Flight over North East Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6671,
                "startTime": "2011-04-04T23:00:00",
                "endTime": "2011-04-05T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24585,
            "uuid": "3b947e30d5d1484290141452f0198656",
            "short_code": "mpop",
            "title": "ARSF 2011_097 - EUFAR HYMEDECOS-GRADIENTS/EUFAR11_04 Flight: flight details over Alentejo region, southern Portugal",
            "abstract": "Flight details for ARSF 2011_097 - EUFAR HYMEDECOS-GRADIENTS/EUFAR11_04 Flight over Alentejo region, southern Portugal. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6672,
                "startTime": "2011-04-06T23:00:00",
                "endTime": "2011-04-07T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24590,
            "uuid": "8d101917340444c18594bc9c0c8c9be9",
            "short_code": "mpop",
            "title": "ARSF 2011_220 - EUFAR SEDMEDHY/EUFAR11_07 Flight: flight details over Toledo, Spain",
            "abstract": "Flight details for ARSF 2011_220 - EUFAR SEDMEDHY/EUFAR11_07 Flight over Toledo, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6673,
                "startTime": "2011-08-07T23:00:00",
                "endTime": "2011-08-08T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24595,
            "uuid": "21a55d8c22ea4bd396420b78742f7750",
            "short_code": "mpop",
            "title": "ARSF 2011_222 - EUFAR SEDMEDHY/EUFAR11_07 Flight: flight details over Toledo, Spain",
            "abstract": "Flight details for ARSF 2011_222 - EUFAR SEDMEDHY/EUFAR11_07 Flight over Toledo, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6674,
                "startTime": "2011-08-09T23:00:00",
                "endTime": "2011-08-10T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24599,
            "uuid": "3d58c5f251ef4251a4bffdbb31dfad41",
            "short_code": "mpop",
            "title": "ARSF 2011_187 - EUFAR SVALBD-PGLACIAL2/EUFAR11_02 Flight: flight details over Ny-Alesund, Svalbard, Norway",
            "abstract": "Flight details for ARSF 2011_187 - EUFAR SVALBD-PGLACIAL2/EUFAR11_02 Flight over Ny-Alesund, Svalbard, Norway. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6675,
                "startTime": "2011-07-05T23:00:00",
                "endTime": "2011-07-06T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24604,
            "uuid": "1eb19301f7c24780909d71ba812c0ab1",
            "short_code": "mpop",
            "title": "ARSF 2011_098 - EUFAR DEINVADER/EUFAR11_06 Flight: flight details over Southwest Portugal",
            "abstract": "Flight details for ARSF 2011_098 - EUFAR DEINVADER/EUFAR11_06 Flight over Southwest Portugal. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6676,
                "startTime": "2011-04-07T23:00:00",
                "endTime": "2011-04-08T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24609,
            "uuid": "c9e01e27e12e4d9480f839470d85c180",
            "short_code": "mpop",
            "title": "ARSF 2012_240a - EUFAR ICELAND_DEBRISFLOWS/EUFAR12_02 Flight: flight details over Sugandafjorour and Skutulsfjorour in the Westfjords, Iceland",
            "abstract": "Flight details for ARSF 2012_240a - EUFAR ICELAND_DEBRISFLOWS/EUFAR12_02 Flight over Sugandafjorour and Skutulsfjorour in the Westfjords, Iceland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6677,
                "startTime": "2012-08-26T23:00:00",
                "endTime": "2012-08-27T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24614,
            "uuid": "27343d1496a546c496e729a7308bc99e",
            "short_code": "mpop",
            "title": "ARSF 2012_240b - EUFAR ICELAND_DEBRISFLOWS/EUFAR12_02 Flight: flight details over Sugandafjorour and Skutulsfjorour in the Westfjords, Iceland",
            "abstract": "Flight details for ARSF 2012_240b - EUFAR ICELAND_DEBRISFLOWS/EUFAR12_02 Flight over Sugandafjorour and Skutulsfjorour in the Westfjords, Iceland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6678,
                "startTime": "2012-08-26T23:00:00",
                "endTime": "2012-08-27T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24618,
            "uuid": "b71d34089d9b472c8a570c8c743a89dd",
            "short_code": "mpop",
            "title": "ARSF 2015_270 - EUFAR HYMOSENS2/EUFAR15_68 Flight: flight details over Ain, France",
            "abstract": "Flight details for ARSF 2015_270 - EUFAR HYMOSENS2/EUFAR15_68 Flight over Ain, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6679,
                "startTime": "2015-09-26T23:00:00",
                "endTime": "2015-09-27T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24623,
            "uuid": "f38d476f26a74e2d8ed898c3917c1e76",
            "short_code": "mpop",
            "title": "ARSF 2015_272 - EUFAR HYMOSENS2/EUFAR15_68 Flight: flight details over Ain, France",
            "abstract": "Flight details for ARSF 2015_272 - EUFAR HYMOSENS2/EUFAR15_68 Flight over Ain, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6680,
                "startTime": "2015-09-28T23:00:00",
                "endTime": "2015-09-29T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24627,
            "uuid": "43ac27316005408fa82e2feb9316efd2",
            "short_code": "mpop",
            "title": "ARSF 2015_244b - EUFAR HOLUHRAUN_HAZ/EUFAR15_58 Flight: flight details over Central Iceland",
            "abstract": "Flight details for ARSF 2015_244b - EUFAR HOLUHRAUN_HAZ/EUFAR15_58 Flight over Central Iceland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6681,
                "startTime": "2015-08-31T23:00:00",
                "endTime": "2015-09-01T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24632,
            "uuid": "c42712e6d5d546f9888f740c132bea6d",
            "short_code": "mpop",
            "title": "ARSF 2015_247a - EUFAR HOLUHRAUN_HAZ/EUFAR15_58 Flight: flight details over Central Iceland",
            "abstract": "Flight details for ARSF 2015_247a - EUFAR HOLUHRAUN_HAZ/EUFAR15_58 Flight over Central Iceland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6682,
                "startTime": "2015-09-03T23:00:00",
                "endTime": "2015-09-04T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24636,
            "uuid": "f6722cb4c43741f7b95d9c408564f3b9",
            "short_code": "mpop",
            "title": "ARSF 2015_249 - EUFAR HIDHAZ_N_ICELAND/EUFAR15_48 Flight: flight details over Mafellshyrna, Iceland",
            "abstract": "Flight details for ARSF 2015_249 - EUFAR HIDHAZ_N_ICELAND/EUFAR15_48 Flight over Mafellshyrna, Iceland. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6683,
                "startTime": "2015-09-05T23:00:00",
                "endTime": "2015-09-06T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24641,
            "uuid": "768aafa2be88414993e0c9768b3a98bb",
            "short_code": "mpop",
            "title": "ARSF 2015_169a - EUFAR MEDHY2CON/EUFAR15_38 Flight: flight details over Mallorca, Spain",
            "abstract": "Flight details for ARSF 2015_169a - EUFAR MEDHY2CON/EUFAR15_38 Flight over Mallorca, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6684,
                "startTime": "2015-06-17T23:00:00",
                "endTime": "2015-06-18T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24646,
            "uuid": "825936ee8b9e4956a32f689cdd2d1a8b",
            "short_code": "mpop",
            "title": "ARSF 2015_169b - EUFAR MEDHY2CON/EUFAR15_38 Flight: flight details over Mallorca, Spain",
            "abstract": "Flight details for ARSF 2015_169b - EUFAR MEDHY2CON/EUFAR15_38 Flight over Mallorca, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6685,
                "startTime": "2015-06-17T23:00:00",
                "endTime": "2015-06-18T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24650,
            "uuid": "f49ad09dc37443d3a8c9d491fe53c911",
            "short_code": "mpop",
            "title": "ARSF 2015_170 - EUFAR MEDHY2CON/EUFAR15_38 Flight: flight details over Mallorca, Spain",
            "abstract": "Flight details for ARSF 2015_170 - EUFAR MEDHY2CON/EUFAR15_38 Flight over Mallorca, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6686,
                "startTime": "2015-06-18T23:00:00",
                "endTime": "2015-06-19T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24654,
            "uuid": "61f7f81367d241f1a42291fcdf4832f3",
            "short_code": "mpop",
            "title": "ARSF 2015_268 - EUFAR MEDHY2CON/EUFAR15_38 Flight: flight details over Mallorca, Spain",
            "abstract": "Flight details for ARSF 2015_268 - EUFAR MEDHY2CON/EUFAR15_38 Flight over Mallorca, Spain. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6687,
                "startTime": "2015-09-24T23:00:00",
                "endTime": "2015-09-25T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24658,
            "uuid": "b785c4e0781c45a8a8a5fd685309fb71",
            "short_code": "mpop",
            "title": "ARSF 2015_174 - EUFAR AHSPECT/EUFAR15_18 Flight: flight details over Toulouse, France",
            "abstract": "Flight details for ARSF 2015_174 - EUFAR AHSPECT/EUFAR15_18 Flight over Toulouse, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6688,
                "startTime": "2015-06-22T23:00:00",
                "endTime": "2015-06-23T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24663,
            "uuid": "afbe3075a694440f88a27d6d4515a8ba",
            "short_code": "mpop",
            "title": "ARSF 2015_274 - EUFAR AHSPECT/EUFAR15_18 Flight: flight details over Toulouse, France",
            "abstract": "Flight details for ARSF 2015_274 - EUFAR AHSPECT/EUFAR15_18 Flight over Toulouse, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6689,
                "startTime": "2015-09-30T23:00:00",
                "endTime": "2015-10-01T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24667,
            "uuid": "96618fa5d8094f90b99936d87dea4b6b",
            "short_code": "mpop",
            "title": "ARSF 2015_175a - EUFAR ISOTHERM/EUFAR15_28 Flight: flight details over Mont Blanc, France",
            "abstract": "Flight details for ARSF 2015_175a - EUFAR ISOTHERM/EUFAR15_28 Flight over Mont Blanc, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6690,
                "startTime": "2015-06-23T23:00:00",
                "endTime": "2015-06-24T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24672,
            "uuid": "fa9dd63348404d67a2a298f6733a2f10",
            "short_code": "mpop",
            "title": "ARSF 2015_175b - EUFAR ISOTHERM/EUFAR15_28 Flight: flight details over Mont Blanc, France",
            "abstract": "Flight details for ARSF 2015_175b - EUFAR ISOTHERM/EUFAR15_28 Flight over Mont Blanc, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6691,
                "startTime": "2015-06-23T23:00:00",
                "endTime": "2015-06-24T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24676,
            "uuid": "8d10882d378244c4898189ce85f1c388",
            "short_code": "mpop",
            "title": "ARSF 2015_271a - EUFAR ISOTHERM/EUFAR15_28 Flight: flight details over Mont Blanc, France",
            "abstract": "Flight details for ARSF 2015_271a - EUFAR ISOTHERM/EUFAR15_28 Flight over Mont Blanc, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6692,
                "startTime": "2015-09-27T23:00:00",
                "endTime": "2015-09-28T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24680,
            "uuid": "3cf6459aa3e541b4b556456aac489718",
            "short_code": "mpop",
            "title": "ARSF 2015_271b - EUFAR ISOTHERM/EUFAR15_28 Flight: flight details over Mont Blanc, France",
            "abstract": "Flight details for ARSF 2015_271b - EUFAR ISOTHERM/EUFAR15_28 Flight over Mont Blanc, France. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 6394,
                "uuid": "d2c5c36981824b71a98a2906394d61f3",
                "short_code": "plat",
                "title": "NERC ARSF Dornier Do228-101 D-CALM Aircraft",
                "abstract": "NERC leased Dornier 228 twin prop converted airliner\r\n\r\nDornier 228 D-CALM is a medium tropospheric research aircraft operated by NERC, UK. It has a twin turbo-prop powered non-pressurised shoulder-wing monoplane with rectangular-section fuselage and a double passenger/cargo door. The aircraft is used in the fields of optical remote sensing, oceanography, atmospheric and earth science research. A range of sensors may be installed.\r\n\r\nDimensions:\r\n\r\n      Length: 15.04 m; Height: 4.86 m; Wingspan: 16.87 m; \r\n\r\n\r\nFlying performances:\r\n\r\n      Speed:\r\n            Min speed: 62 m/s\r\n            Max speed: 83 m/s\r\n            Usual speed during measurements: 65 m/s\r\n            Usual speed during transit flights: 98 m/s\r\n            Ascent rate: 1000 m/s\r\n\r\n      Altitude:\r\n      (1 ft = 0.31 m)\r\n            Min altitude:\r\n                  Above sea: 200 ft\r\n                  Above ground: 500 ft\r\n            Max ceiling: 22000 ft\r\n            Usual ceiling during measurements: 15000 ft\r\n            Ceiling limitations:\r\n                  The service ceiling for our normal operational science is 15 000ft. However, our maximum service ceiling is 22 000ft, dependent on crew oxygen and specific instrument hard-drive specifications. \r\n\r\n      Payload:\r\n            Empty weight: 3596 kg\r\n            Max take-off weight: 5980 kg\r\n            Max payload: 1595 kg\r\n            Usual scientific payload during measurements: 500 kg\r\n      Endurance:\r\n            Max endurance: 7 h (at min scientific payload and max fuel) (Y-coordinate of 1st point)\r\n            Endurance at max scientific payload: 5 h ... (Y-coordinate of 2nd point)\r\n      \t\r\n      Range:\r\n            Max range: 2600 km (at min scientific payload and max fuel)\r\n            Conditions for max range:\r\n                  FL150 at max fuel, speed = 180 KTAS\r\n            Range at max scientific payload: 1800 km\r\n            Usual range during measurement flight: 1500 km\r\n\r\n      Other:\r\n            Weather conditions limitations:\r\n                  VFR/IFR Approved Certified to fly in known icing conditions\r\n            Take-off runway length: 625 m\r\n            Engines:\r\n                  twin turbo-prop: Garrett TPE 331-5A-252 D with 533 kW (715 SHP) take-off power.;\r\n            Avionics:\r\n                  INS, GPS, Transponder, DME, Weather radar, radio-altimeter \r\n\r\nCrew and scientists on board:\r\n\r\n      Crew (pilots + operators): VFR: 1 pilotIFR: 2 pilots;\r\n      Seats available for scientists: 1 operator seat, 3 potentially\r\n\r\nCabin:\r\n\r\n\r\n      Apertures:\r\n            Cargo door:\r\n            Width : 1.28 m\r\n            Height : 1.34 m;\r\n      Cabin pressurized:\r\n            none\r\n      More information:\r\n            Flexible accommodation for standard 19-inch racking, secured via the seat-rails.\r\n\r\n            See below for additional information; \r\n\r\nAircraft modifications:\r\n\r\n      Nose boom:\r\n            none\r\n      Windows:\r\n            2 Bubble-window with operator position and floor-opening for navigation-sight at the right forward side of the cabin\r\n      Openings:\r\n            Cabin floor, Back. One 2060 mm x 515 mm (frame 20 to 25) and one approx. 425mm diam (frame 25 to 27).\r\n            Covered openings in the cabin roof - 400 mm diam back (between frame 23 and 24) - 150 mm diam fromt (frame 12/13) - 150 mm diam back(frame 22/23)\r\n      Hard points:\r\n            Six hardpoints below the cockpit-area for external loads up to 200 Kg- Each fuselage side (cockpit area) has three hardpoint\r\n            -pairs to carry a load of 50 Kg (e.g. SLAR-antennae).\r\n            -On both wings (outside of propwash) two wing-stations for external loads up to 100kg\r\n      Inlets:\r\n            One, installed on cabin roof aperture (frame 12/13), to accommodate Aerosol and/or whole-air inlets\r\n      Additional systems:\r\n            From the wing-stations to the cabin there are tubes for cables (power and data lines) pylons/pods to carry four Particle Measurement Systems (PMS) type probes. \r\n\r\nAcquisition systems:\r\n\r\n      Leica ALS 50-II Lidar\r\n      Leica RCD-105 39 Mega Pixel Digital Camera\r\n      Specim Eagle & Hawk Hyperspectral Scanner\r\n      Applanix POS and IPAS - Attitude and position\r\n\r\nElectrical power:\r\n\r\n      Aircraft total electrical power (kW):\r\n            28V DC, 8.4 kW , 220 V AC, 2kW, 50 Hz \r\n      Electrical power (kW) and voltages (V) available for scientists:\r\n            DC 28 V – 6.3 kW of 28 volt DC total power, including a permanently installed 1.6kW / 220 V / 50 Hz inverter "
            },
            "location": null,
            "operationTime": {
                "ob_id": 6693,
                "startTime": "2015-09-27T23:00:00",
                "endTime": "2015-09-28T22:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24722,
            "uuid": "533d1cb20d324f9794a04956c25cf912",
            "short_code": "mpop",
            "title": "FAAM BAE-147 flight B992",
            "abstract": "Flight details for FAAM BAE-146 aircraft flight number B992. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "location": {
                "ob_id": 1746,
                "bboxName": "",
                "eastBoundLongitude": 2.099541425704956,
                "westBoundLongitude": -1.1598962545394897,
                "southBoundLatitude": 52.035465240478516,
                "northBoundLatitude": 55.231014251708984
            },
            "operationTime": {
                "ob_id": 6702,
                "startTime": "2017-01-19T08:28:48",
                "endTime": "2017-01-19T16:37:29"
            },
            "childOperation": null
        },
        {
            "ob_id": 24726,
            "uuid": "cf2a521c314047da94b26eef03090587",
            "short_code": "mpop",
            "title": "FAAM BAE-147 flight B993",
            "abstract": "Flight details for FAAM BAE-146 aircraft flight number B993. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6703,
                "startTime": "2017-01-20T08:45:53",
                "endTime": "2017-01-20T15:08:57"
            },
            "childOperation": null
        },
        {
            "ob_id": 24730,
            "uuid": "4f91fd93ed3141828de4f2873361c2ce",
            "short_code": "mpop",
            "title": "FAAM BAE-147 flight B994",
            "abstract": "Flight details for FAAM BAE-146 aircraft flight number B994. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6704,
                "startTime": "2017-02-03T08:14:07",
                "endTime": "2017-02-03T14:30:38"
            },
            "childOperation": null
        },
        {
            "ob_id": 24734,
            "uuid": "81e7e88e75db452cbac85d50349e74f7",
            "short_code": "mpop",
            "title": "FAAM BAE-147 flight B995",
            "abstract": "Flight details for FAAM BAE-146 aircraft flight number B995. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6705,
                "startTime": "2017-02-08T08:30:12",
                "endTime": "2017-02-08T15:29:43"
            },
            "childOperation": null
        },
        {
            "ob_id": 24739,
            "uuid": "3f6d324c95974bac8657396cd7039b16",
            "short_code": "mpop",
            "title": "FAAM BAE-147 flight B996",
            "abstract": "Flight details for FAAM BAE-146 aircraft flight number B996. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6706,
                "startTime": "2017-02-13T05:49:22",
                "endTime": "2017-02-13T13:20:57"
            },
            "childOperation": null
        },
        {
            "ob_id": 24743,
            "uuid": "8496e7df13344ad19264df2c54d91cd3",
            "short_code": "mpop",
            "title": "FAAM BAE-147 flight B997",
            "abstract": "Flight details for FAAM BAE-146 aircraft flight number B997. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6707,
                "startTime": "2017-02-13T14:36:06",
                "endTime": "2017-02-13T19:11:22"
            },
            "childOperation": null
        },
        {
            "ob_id": 24747,
            "uuid": "8b23553027dc4798bf3833268e9ae34f",
            "short_code": "mpop",
            "title": "FAAM BAE-147 flight B998",
            "abstract": "Flight details for FAAM BAE-146 aircraft flight number B998. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6708,
                "startTime": "2017-02-14T09:54:28",
                "endTime": "2017-02-14T18:01:04"
            },
            "childOperation": null
        },
        {
            "ob_id": 24751,
            "uuid": "48c8703ff906475f945393f07ccd0b4c",
            "short_code": "mpop",
            "title": "FAAM BAE-147 flight B999",
            "abstract": "Flight details for FAAM BAE-146 aircraft flight number B999. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6709,
                "startTime": "2017-02-15T10:28:16",
                "endTime": "2017-02-15T17:09:27"
            },
            "childOperation": null
        },
        {
            "ob_id": 24755,
            "uuid": "c6e072461cf94fb29e58493197610d62",
            "short_code": "mpop",
            "title": "FAAM BAE-147 flight C001",
            "abstract": "Flight details for FAAM BAE-146 aircraft flight number C001. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6710,
                "startTime": "2017-02-16T00:00:00",
                "endTime": "2017-02-16T23:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24759,
            "uuid": "b8cfc8d632f346a08d0dd04ffd3d05ad",
            "short_code": "mpop",
            "title": "FAAM BAE-147 flight C002",
            "abstract": "Flight details for FAAM BAE-146 aircraft flight number C002. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "location": null,
            "operationTime": {
                "ob_id": 6711,
                "startTime": "2017-02-16T00:00:00",
                "endTime": "2017-02-16T23:59:59"
            },
            "childOperation": null
        },
        {
            "ob_id": 24764,
            "uuid": "387aa3feb7bf491396c1d185989cce55",
            "short_code": "mpop",
            "title": "FAAM BAE-147 flight C003",
            "abstract": "Flight details for FAAM BAE-146 aircraft flight number C003. See linked documentation for further details.",
            "status": "completed",
            "platform_field": {
                "ob_id": 51,
                "uuid": "dda4596d5d374564acf8c79b7a119127",
                "short_code": "plat",
                "title": "FAAM BAe-146-301 Large Atmospheric Research Aircraft G-LUXE",
                "abstract": "FAAM is the result of a collaboration between the Met Office(TM) and the Natural Environment Research Council (NERC) and has been established as part of the National Centre for Atmospheric Science (NCAS) to provide an aircraft measurement platform for use by all the UK atmospheric research community on campaigns throughout the world. The modified BAE 146 aircraft (jet type) is owned by BAE Systems and operated for them by Directflight. The Home Base is at Cranfield University, Bedfordshire.\r\n\r\nThe FAAM BAE 146 aircraft allows for in-situ measurements taken by core and non-core instruments onboard the aircraft. The in-situ measurements will then be transported to the research organisations' respective laboratory for analysis"
            },
            "location": null,
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