An experimental investigation was conducted to determine the feasibility and practicality of the dual chamber rocket concept. Cold flow studies were performed which utilized a telescoping booster cavity. The effects of booster cavity length, booster cavity shockdown pressure, booster/sustainer nozzle area ratio, and aft nozzle removal on thrust and the booster cavity pressure distribution were explored. (Author)


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    Title :

    An Experimental Investigation of the Dual Chamber Rocket


    Contributors:

    Publication date :

    1979


    Size :

    48 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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