Wind tunnel tests to determine static aerodynamic characteristics of space shuttle booster configuration at subsonic speeds


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    Title :

    Space shuttle: Static aerodynamic characteristics of the Boeing space shuttle booster configuration at Mach 0.10 to 0.29


    Contributors:
    Houser, J. (author)

    Publication date :

    1971-07-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :