A passive propellant acquisition and feed system is disclosed which acquires and feeds gas-free propellant in low or zero-g environments during orbital maneuvers and retains this propellant under high axially directed acceleration such as may be experienced during launch of a space vehicle and orbit-to-orbit transfer is described. The propellant system includes a dual compartment propellant tank with independent surface tension acquisition channels in each compartment to provide gas-free flow of pressurized liquid propellant from one compartment to the other in one direction only.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Passive Propellant System


    Beteiligte:
    D. A. Hess (Autor:in) / W. W. Regnier (Autor:in) / V. L. Jacobs (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Passive propellant system

    Hess, D. A. / Regnier, W. W. / Jacobs, V. L. | NTRS | 1979


    Passive propellant system

    Hess, D. A. / Regnier, W. W. / Jacobs, V. L. | NTRS | 1978


    Passive Propellant System

    D. A. Hess / W. W. Regnier / V. L. Jacobs | NTIS | 1978


    Criteria for passive propellant control schemes.

    Barksdale, T. R. / Paynter, H. L. | NTRS | 1969