An experimental investigation was conducted to determine the feasibility and practicality of the dual rocket motor concept. Cold flow studies were performed with the aid of a ground-test simulator which incorporated a telescoping booster cavity. The effects of booster cavity length, booster cavity shockdown pressure, booster/sustainer nozzle area ratios, and aft nozzle removal on thrust and performance were explored and discussed. (Author)


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    Title :

    An Experimental Investigation of the Dual Chamber Rocket


    Contributors:

    Publication date :

    1978


    Size :

    55 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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