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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    Title :

    Space Shuttle External Tank Instrumentation Evaluation


    Contributors:

    Publication date :

    1979


    Size :

    33 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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