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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    Titel :

    ANTRIEBSSTUFE EINER TRÄGERRAKETE, TRÄGERRAKETE UND VERFAHREN ZUM STEUERN EINER ANTRIEBSSTUFE


    Weitere Titelangaben:

    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


    Beteiligte:
    LARCH SASCHA (Autor:in)

    Erscheinungsdatum :

    19.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Deutsch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / B64C AEROPLANES , Flugzeuge






    Trägerrakete und Verfahren zum Betreiben einer Trägerrakete

    LARCH SASCHA | Europäisches Patentamt | 2022

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