A wind tunnel test of the space shuttle orbiter configuration 040A was run in a 20 in. supersonic wind tunnel. Basic aerodynamic data for this vehicle were determined at Mach 2.0, 2.4, 3.0 and 4.0.


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    Title :

    Space shuttle: Supersonic aerodynamic characteristics of the MSC 040A orbiter (M equals 2.0 to 4.0)


    Contributors:
    Tessitore, F. (author) / Quan, M. (author) / Romere, R. (author) / Moore, R. (author) / Weaver, R. (author)

    Publication date :

    1972-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :