The invention pertains to a regeneratively cooled thrust chamber of a liquid propellant rocket engine and, more specifically, to the structure of the wall of the thrust chamber and to a method of manufacturing the wall.


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    Title :

    Composite Wall for a Regeneratively Cooled Thrust Chamber of a Liquid Propellant Rocket Engine


    Contributors:
    D. H. Huang (author)

    Publication date :

    1973


    Size :

    21 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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