Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at supersonic and hypersonic speeds


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    Title :

    Wind tunnel investigation of three proposed launch vehicles at Mach numbers from 2.30 to 4.63


    Contributors:

    Publication date :

    1968-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :