A space vehicle engine (10) comprising a chemical thruster having a nozzle (30) for ejecting combustion gas, together with a Hall effect thruster. The engine is arranged in such a manner that the nozzle serves as the ejection channel for particles ejected by the Hall effect thruster when it is in operation. The engine can deliver high thrust with low specific impulse or relatively low thrust with large specific impulse.


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    Title :

    MOTEUR POUR ENGIN SPATIAL, ET ENGIN SPATIAL COMPRENANT UN TEL MOTEUR


    Additional title:

    ENGINE FOR A SPACECRAFT, AND SPACECRAFT COMPRISING SUCH AN ENGINE
    MOTOR FÜR EIN RAUMFAHRZEUG UND RAUMFAHRZEUG MIT SOLCH EINEM MOTOR



    Publication date :

    2020-07-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F03H PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR , Erzeugung von Vortriebskraft [Schub] nach dem Prinzip des Rückstoßes, soweit nicht anderweitig vorgesehen / B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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