Wind tunnel tests were performed to determine the static aerodynamic characteristics of a model of a 60 degree swept delta wing space shuttle orbiter. Some control effectiveness tests were included. The tests were conducted in a unitary plan wind tunnel at Mach numbers of 2.50, 3.90, and 4.60. (Author)


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    Title :

    Aerodynamic Characteristics of a 60 Degree Swept delta-Wing Space Shuttle Orbiter at Mach Numbers of 2.50, 3.90, AND 4.60


    Contributors:

    Publication date :

    1972


    Size :

    116 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English