This paper discusses the engine system and component design of the J-2 liquid propellant rocket engine, with emphasis upon the newer features whose development has been dictated by the use of liquid hydrogen as the fuel. A brief description of the development program and of the principal specialized test equipment is given.


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    Title :

    The J-2 Liquid Hydrogen Rocket Engine


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    SAE World Congress & Exhibition ; 1964



    Publication date :

    1964-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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