A method in a spacecraft for transporting propellant to be consumed by a thruster includes storing the propellant in the spacecraft in a solid state during at least a portion of a take-off procedure and supplying the propellant to the thruster in a liquid or vaporous state when the spacecraft is in space.


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    Titel :

    Spacecraft Structures and Mechanisms


    Beteiligte:
    PARMAN MATTHEW (Autor:in) / SERCEL JOEL (Autor:in) / KOKORICH MIKHAIL (Autor:in) / SMALL JAMES (Autor:in) / SIMON NICHOLAS (Autor:in) / ORR NATHAN (Autor:in) / AVERY SAMUEL (Autor:in) / STANLEY SCOTT (Autor:in)

    Erscheinungsdatum :

    17.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    SPACECRAFT STRUCTURES AND MECHANISMS

    PARMAN MATTHEW / SERCEL JOEL / KOKORICH MIKHAIL et al. | Europäisches Patentamt | 2020

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