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.


    Access

    Download


    Export, share and cite



    Title :

    RETURN TO BASE SPACE LAUNCH VEHICLES, SYSTEMS AND METHODS


    Additional title:

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


    Contributors:

    Publication date :

    2020-05-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Return to base space launch vehicles, systems and methods

    ARGEMI SAMSO ADRIA / BERGSTROM RASMUS / ROSSI FEDERICO et al. | European Patent Office | 2024

    Free access

    RETURN TO BASE SPACE LAUNCH VEHICLES, SYSTEMS AND METHODS

    ARGEMI SAMSO ADRIA / BERGSTROM RASMUS / ROSSI FEDERICO et al. | European Patent Office | 2020

    Free access

    RETURN TO BASE SPACE LAUNCH VEHICLES, SYSTEMS AND METHODS

    ARGEMI SAMSO ADRIA / BERGSTROM RASMUS / ROSSI FEDERICO et al. | European Patent Office | 2022

    Free access


    Launch Systems for Space Vehicles

    E. Schaefer | NTIS | 1967