Static longitudinal aerodynamic characteristics of configurations used in Little Joe/Apollo test vehicle development


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    Title :

    Static longitudinal aerodynamic characteristics of several configurations used in the development of the Little Joe 2-Apollo test vehicle at Mach numbers from 0.056 to 4.65


    Contributors:

    Publication date :

    1968-05-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :