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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    Title :

    SPACECRAFT THERMAL AND FLUID MANAGEMENT SYSTEMS


    Contributors:
    KOKORICH MIKHAIL (author) / SERCEL JOEL (author) / MITCHELL AARON (author) / MINSTER GEDI (author) / WANG YUQI (author) / WILSON LEE (author) / SMALL JAMES (author)

    Publication date :

    2020-09-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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



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    KOKORICH MIKHAIL / SERCEL JOEL / MITCHELL AARON et al. | European Patent Office | 2020

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    SPACECRAFT THERMAL AND FLUID MANAGEMENT SYSTEMS

    KOKORICH MIKHAIL / SERCEL JOEL / MITCHELL AARON et al. | European Patent Office | 2022

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    Design assistant for spacecraft thermal management systems

    Fox, B.R. / Brewster, L.T. / Kher, R.P. et al. | Tema Archive | 1985


    Weight characteristics of future spacecraft thermal management systems

    SHEFFIELD, J. / VAN GRIETHUYSEN, V. | AIAA | 1984