An evaluation is presented of J-2 engine modifications that will simplify operation and improve reliability of the advanced Saturn 1C launch vehicle. Methods of increasing thrust without extensively modifying the S-2 or S-4B stages are also evaluated. A thrust increase was achieved by raising engine combustion through a redesign of the engine thrust chamber and propellant feed system.


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    Title :

    Extendible rocket nozzle development


    Contributors:
    Pryor, D. (author)


    Publication date :

    1972-08-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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