Platform Instance

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{
    "ob_id": 6399,
    "uuid": "53ebb1bb71414347be1c2221894b2653",
    "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.",
    "keywords": "EUFAR aircraft ",
    "identifier_set": [
        "https://api.catalogue.ceda.ac.uk/api/v2/identifiers/4200/?format=api",
        "https://api.catalogue.ceda.ac.uk/api/v2/identifiers/4199/?format=api",
        "https://api.catalogue.ceda.ac.uk/api/v2/identifiers/9149/?format=api"
    ],
    "platformType": "aircraft",
    "parentPlatform": [],
    "childPlatform": [],
    "responsiblepartyinfo_set": [
        "https://api.catalogue.ceda.ac.uk/api/v2/rpis/27962/?format=api",
        "https://api.catalogue.ceda.ac.uk/api/v2/rpis/27961/?format=api"
    ]
}