The design of cryogenic flow control components, specifically the prevalve, for the Saturn 5 vehicle is discussed. Design systems are assessed and component requirements revealed significant improvements in mass flow rate, temperature, and pressure.


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    Titel :

    Cryogenic flow control components for rocket propulsion systems


    Beteiligte:
    Potter, J. H. (Autor:in)


    Erscheinungsdatum :

    01.08.1972


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Structural Analysis of Propulsion System Components of an Indigenous Cryogenic Rocket Engine

    Asraff, A. / Muthukumar, R. / Ramnathan, T. et al. | AIAA | 2008


    METHOD OF PREPARING ROCKET FUEL COMPONENTS FOR REFUELING ROCKET PROPULSION SYSTEMS

    GORYAEV ANDREJ NIKOLAEVICH / NAZARENKO VADIM VADIMOVICH / KISELEV ALEKSANDR PETROVICH et al. | Europäisches Patentamt | 2017

    Freier Zugriff


    Rocket propulsion

    Dunn, L.G. | Engineering Index Backfile | 1947


    Rocket Propulsion

    Springer Verlag | 2007