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

    Erscheinungsdatum :

    1966


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Supercharged topping rocket propellant feed system

    Stewart, W. L. / Ginsburg, A. / Hartmann, M. J. | NTRS | 1979




    Rocket propellant manometer system

    Kreisler, R.I. | Engineering Index Backfile | 1962