Wind tunnel tests to determine aerodynamic characteristics of booster and ascent shuttle configuration from Mach 0.28 to 10.4


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    Title :

    Aerodynamic characteristics of a booster and an ascent shuttle configuration from Mach 0.28 to Mach 10.4


    Contributors:

    Publication date :

    1971-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :