A stage (10) for a space launch vehicle (1) is provided. The space launch vehicle has a main body including a first end (14) and a second end (16), and defines a central longitudinal axis (12) between the first end and the second end. The stage comprises a stage rocket engine (11) arranged at or near the first end of the stage to propel the launch vehicle vertically upwards at take-off. The stage furthermore comprises a plurality of fans (18) for providing lift during a landing procedure of the stage, wherein the fans have a rotational axis arranged substantially perpendicular to the central longitudinal axis. Also provided are space launch vehicles and methods for transporting a payload into space.


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    Titel :

    RETURN TO BASE SPACE LAUNCH VEHICLES, SYSTEMS AND METHODS


    Weitere Titelangaben:

    RAUMFAHRTTRÄGERRAKETE MIT RÜCKKEHR ZUR BASIS, SYSTEME UND VERFAHREN
    VÉHICULES, SYSTÈMES ET PROCÉDÉS DE LANCEMENT DANS L'ESPACE DE RETOUR À LA BASE


    Beteiligte:

    Erscheinungsdatum :

    13.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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