A rocket propellant injector is provided in which all of the fuel flows through a porous faceplate for transpiration cooling. The oxidizer is swirled in tubular elements extending through the faceplate.


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    Title :

    Rocket Propellant Injection


    Contributors:
    G. A. Repas (author)

    Publication date :

    1973


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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