A propulsion stage, in particular a reusable propulsion stage, comprising: a rocket body having a longitudinal axis; at least one recoil propulsion unit acting substantially parallel to the longitudinal axis; a plurality of rotor assemblies, each drivable by an electric rotor drive including at least one electric motor electrically connected to at least one current storage device configured to supply electrical energy to the at least one electric motor, wherein the at least one current storage device is displaceable within the propulsion stage in a direction located in a plane oriented at a right angle relative to the longitudinal axis or which has a dominant directional component which extends in the radial direction at a right angle relative to the longitudinal axis.


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    Title :

    ANTRIEBSSTUFE EINER TRÄGERRAKETE, TRÄGERRAKETE UND VERFAHREN ZUM STEUERN EINER ANTRIEBSSTUFE


    Additional title:

    PROPULSION STAGE OF A LAUNCH VEHICLE, LAUNCH VEHICLE AND METHOD FOR CONTROLLING A PROPULSION STAGE
    ÉTAGE DE PROPULSION D'UN VÉHICULE DE LANCEMENT, VÉHICULE DE LANCEMENT ET PROCÉDÉ DE COMMANDE D'UN ÉTAGE DE PROPULSION


    Contributors:

    Publication date :

    2025-03-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / B64C AEROPLANES , Flugzeuge