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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    Titel :

    Experimental investigation of a lightweight rocket chamber


    Beteiligte:

    Erscheinungsdatum :

    01.10.1953


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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