Wind tunnel stability tests of space shuttle model booster with G3-A orbiter


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    Title :

    Space shuttle: Aerodynamic stability and control characteristics of a TBC space shuttle booster and GAC orbiter, M equal 0.6 to 4.96


    Contributors:
    Johnson, J. (author) / Watts, L. L. (author)

    Publication date :

    1971-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :