This specification established the requirements for a 5 second duration, 4500 pound thrust (when determined at 60°F) solid propellant rocket engine hereinafter specified as 5 S-4500.


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    Title :

    Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust


    Publication date :

    2000-03-01



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English







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