Data were obtained on the performance of space shuttle flight instrumentation under simulated flight conditions. These conditions included ablating insulation material. The tests were conducted at a free-stream Mach number of 10 and tunnel stilling chamber conditions of 1800 psia and 1900 R. (Author)


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    Titel :

    Space Shuttle External Tank Instrumentation Evaluation


    Beteiligte:

    Erscheinungsdatum :

    1979


    Format / Umfang :

    33 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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