A rocket propulsion system (200, 300, 400, 500, 600) comprising: a propellant tank (208, 306, 308, 406, 408, 506, 508, 606, 608) arranged to contain propellant, a liquid pressurant tank (202, 302, 402, 502a, 602a) arranged to contain a liquid pressurant and to supply the pressurant to the propellant tank to pressurise the propellant tank, an engine (211, 311, 411, 511, 611), the engine comprising: a combustion chamber (210, 310, 410, 510, 610) arranged to receive pressurised propellant from the propellant tank and defining a volume for combusting the pressurised propellant to produce an exhaust product, and an exhaust nozzle (212, 312, 412, 512, 612) arranged to receive the exhaust product from the combustion chamber, and a heat exchanger (214, 314, 414, 514, 614) arranged to transfer heat from the engine to the pressurant.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rocket propulsion system


    Erscheinungsdatum :

    07.04.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Rocket propulsion

    Dunn, L.G. | Engineering Index Backfile | 1947


    Rocket propulsion

    Barrère, Marcel / Jaumotte, André L. / Fraeijs de Veubeke, Baudouin M. et al. | TIBKAT | 1960


    Rocket Propulsion

    Manuel Martinez-Sanchez / Massachusetts Institute of Technology | OERSI

    Freier Zugriff

    Rocket propulsion

    Dunning, J.E.P. | Engineering Index Backfile | 1961


    Rocket Propulsion

    Springer Verlag | 2007