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 :

    23.10.1979


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Supercharged Topping Rocket Propellant Feed System

    W. L. Stewart / A. Ginsburg / M. J. Hartmann | NTIS | 1966



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