A propulsion stage for a launch rocket, the propulsion stage comprising: a rocket body having a longitudinal axis; at least one recoil propulsion unit acting substantially parallel to the longitudinal axis, wherein a liquid propellant is supplyable to the at least one recoil propulsion unit from at least one propellant tank through at least one fuel pump; and a plurality of rotor assemblies, each drivable by a rotor drive including at least one motor, wherein the at least one motor of at least one of the rotor drives is configured to selectively drive at least one of the rotor assemblies and/or the at least one fuel pump of the at least one recoil propulsion unit.


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    Title :

    ANTRIEBSSTUFE EINER TRÄGERRAKETE, TRÄGERRAKETE UND VERFAHREN ZUM BETREIBEN EINER TRÄGERRAKETE


    Additional title:

    PROPULSION STAGE OF A LAUNCH VEHICLE, LAUNCH VEHICLE AND METHOD FOR OPERATING A LAUNCH VEHICLE
    ÉTAGE DE PROPULSION D'UN VÉHICULE DE LANCEMENT, VÉHICULE DE LANCEMENT ET PROCÉDÉ POUR FAIRE FONCTIONNER UN VÉHICULE DE LANCEMENT


    Contributors:

    Publication date :

    2025-03-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS




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