A fuelling system (1) having a fuel supply hose (80) for connecting a launcher (100) and a launch tower (200), wherein the fuel supply hose (80) is configured for conveying a cryogenic medium between the launcher ( 100) and the launch tower (200) and wherein a first end (80.1) of the fuel supply hose (80) is releasably connectable to the launcher (100) such as to release at lift off of the launcher (100) thereby allowing separation of the fuel supply hose (80) from the launcher (100); characterized in that a retraction system (210) is provided for automatically retracting the fuel supply hose (80) upon lift-off of the launcher (100).


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    Titel :

    CRYOGENIC FUELLING SYSTEM


    Weitere Titelangaben:

    SYSTEME D'ALIMENTATION EN COMBUSTIBLE CRYOGENIQUE


    Beteiligte:

    Erscheinungsdatum :

    06.08.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Cryogenic fuelling system

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    Cryogenic fuelling system

    EATON NICHOLAS CHARLES | Europäisches Patentamt | 2016

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    CRYOGENIC FUELLING SYSTEM

    EATON NICHOLAS CHARLES | Europäisches Patentamt | 2015

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    Cryogenic fuelling system

    EATON NICHOLAS CHARLES | Europäisches Patentamt | 2016

    Freier Zugriff

    CRYOGENIC FUELLING SYSTEM

    EATON NICHOLAS CHARLES | Europäisches Patentamt | 2016

    Freier Zugriff