Uplink and downlink telemetry systems were installed in a Boeing 720 aircraft that was remotely flown from Rogers Dry Lake at Edwards Air Force Base and impacted into a designated crash site on the lake bed. The controlled impact demonstration (CID) program was a joint venture by the National Aeronautics and Space Administration (NASA) and the Federal Aviation Administration (FAA) to test passenger survivability using antimisting kerosene (AMK) to inhibit postcrash fires, improve passenger seats and restraints, and improve fire-retardent materials. The uplink telemetry system was used to remotely control the aircraft and activate onboard systems from takeoff until after impact. Aircraft systems for remote control, aircraft structural response, passenger seat and restraint systems, and anthropomorphic dummy responses were recorded and displayed by the downlink stems. The instrumentation uplink and downlink systems are described.


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    Titel :

    Remote control of an impact demonstration vehicle


    Beteiligte:
    Harney, P. F. (Autor:in) / Craft, J. B., Jr. (Autor:in) / Johnson, R. G. (Autor:in)

    Kongress:

    Intern. Instrumentation Symp. of the Instrument Soc. of Am. ; 1985 ; San Diego, CA, United States


    Erscheinungsdatum :

    1985-04-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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