To manage propellant in a spacecraft, the method of this disclosure includes storing propellant in a tank as a mixture of liquid and gas; transferring the propellant out of the tank; converting the mixture of liquid and gas propellant into a single phase, where the single phase is either liquid or gaseous; and supplying the single phase of the propellant to a thruster.


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    Titel :

    SPACECRAFT THERMAL AND FLUID MANAGEMENT SYSTEMS


    Beteiligte:
    KOKORICH MIKHAIL (Autor:in) / SERCEL JOEL (Autor:in) / MITCHELL AARON (Autor:in) / MINSTER GEDI (Autor:in) / WANG YUQI (Autor:in) / WILSON LEE (Autor:in) / SMALL JAMES (Autor:in)

    Erscheinungsdatum :

    2022-06-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / F17C Behälter zum Aufnehmen oder Speichern verdichteter, verflüssigter oder verfestigter Gase , VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES



    SPACECRAFT THERMAL AND FLUID MANAGEMENT SYSTEMS

    KOKORICH MIKHAIL / SERCEL JOEL / MITCHELL AARON et al. | Europäisches Patentamt | 2020

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    SPACECRAFT THERMAL AND FLUID MANAGEMENT SYSTEMS

    KOKORICH MIKHAIL / SERCEL JOEL / MITCHELL AARON et al. | Europäisches Patentamt | 2020

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