An autogenous system for controlling pressurization of a propellant tank in a pressure-fed propulsion system. The system includes at least one micropump that pumps a high vapor pressure liquid propellant or a propellant with low temperature critical point from the propellant tank into an engine in which a small portion of the propellant is evaporated and heated. The micropump controls a pressurization rate of a flow of the propellant. A method of controlling pressurization of a propellant tank in such a system includes pressurizing a propellant tank containing a high vapor pressure liquid propellant or a propellant with low temperature critical point; controlling a flow of a small amount of the propellant from the propellant tank to a combustion chamber using at least one micropump; heating and vaporizing the propellant in a heat exchanger; and using the micropump to control the amount of propellant vaporized and heated, thereby controlling the pressurization rate.


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    Titel :

    MICROPUMP-FED AUTOGENOUS PRESSURIZATION SYSTEM


    Beteiligte:
    BESNARD ERIC G (Autor:in)

    Erscheinungsdatum :

    2018-06-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64G Raumfahrt , COSMONAUTICS



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