A rocket propellant feed system utilizing a bleed turbopump to supercharge a topping turbopump is presented. The bleed turbopump is of a low pressure type to meet the cavitation requirements imposed by the propellant storage tanks. The topping turbopump is of a high pressure type and develops 60 to 70 percent of the pressure rise in the propellant.


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    Titel :

    Supercharged topping rocket propellant feed system


    Beteiligte:
    Stewart, W. L. (Autor:in) / Ginsburg, A. (Autor:in) / Hartmann, M. J. (Autor:in)

    Erscheinungsdatum :

    1979-10-23


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch







    ZERO G PROPELLANT FEED SYSTEMS FOR CESIUM ION ROCKET ENGINES

    BARCATTA, F. / DALEY, H. / FIRESTONE, A. et al. | AIAA | 1963


    Solid-liquid rocket propellant system

    Moore, G.E. / Berman, K. | Engineering Index Backfile | 1956