Jet-stream interaction effects on rocket engine studied with simulated ballistic missile using liquid oxygen and JP-4 fuel mixture


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    Title :

    Experimental investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0


    Contributors:

    Publication date :

    1959-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English