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    Title :

    A Flight Investigation at Mach Numbers from 0.67 to 1.81 of the Longitudinal Stability and Control Characteristics of a 60 Degree Delta-wing Missile Configuration Having an All-movable Tail


    Contributors:

    Publication date :

    1953-10-06


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English