Experiments have been conducted with a jacketed rocket combustion chamber that was fabricated by hydraulic-forming from sheet metal. Rocket combustion chambers made by this method have been used successfully. Runs with these combustion chambers have been made at over-all heat-transfer rates 1.7 Btu per square inch per second with water cooling and also ammonia as a regenerative coolant.


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    Title :

    Experimental investigation of a lightweight rocket chamber


    Contributors:

    Publication date :

    1953-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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