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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    Titel :

    Extendible rocket nozzle development


    Beteiligte:
    Pryor, D. (Autor:in)


    Erscheinungsdatum :

    01.08.1972


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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    Kusaka, K. / Kumakawa, A. / Niino, M. | British Library Conference Proceedings | 2000