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.


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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 :

    1972-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :