A launch system comprises a nose section comprising a nose coupling surface, a tail section comprising a tail coupling surface facing the nose coupling surface and a mast coupling the nose and tail sections. The mast is configured to expand and retract to displace the nose and tail sections within a range of distances from one another. In a retracted state, the nose and tail sections are either structurally coupled to one another at the nose and tail coupling surfaces or structurally coupled to at least one integrated module located between the nose and the tail sections.


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    Titel :

    SPACE SHUTTLE ORBITER AND RETURN SYSTEM


    Weitere Titelangaben:

    RAUMFÄHRENORBITER UND UMKEHRSYSTEM
    ORBITEUR DE NAVETTE SPATIALE ET SYSTÈME DE RETOUR


    Beteiligte:
    HELOU ELIE (Autor:in)

    Erscheinungsdatum :

    24.07.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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