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. (Author)


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    Title :

    Space Shuttle Supersonic Aerodynamic Characteristics of the Msc 040A Orbiter (M Equals 2.0 to 4.0)


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

    Publication date :

    1972


    Size :

    314 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English