Connection module for fuelling a space launch vehicle with cryogenic propellant. The module has a ground part placed on the launch pad mast side of the launch vehicle; a flight part fixed to the launch vehicle; a link fixed to the parts to unite them. The module exhibits a passage crossing the ground part, the flight part and the link. The passage allows communication between a line of the launch pad, such as an umbilical structure of the launch vehicle, and a line supplying a tank or a pneumatic circuit of the launch vehicle. Twisting means, such as a lever or an arm, are linked to a disconnection cable. During lift-off, the twisting means apply a torque to the link which causes the breakage of a link groove, allowing the link to split into two axial portions.


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    Titel :

    MODULE DE RACCORDEMENT D'AVITAILLEMENT POUR LANCEUR SPATIAL


    Weitere Titelangaben:

    REFUELLING CONNECTION MODULE FOR SPACE LAUNCHER
    VERSORGUNGS-ANSCHLUSSMODUL FÜR TRÄGERRAKETE


    Beteiligte:

    Erscheinungsdatum :

    31.10.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F16L PIPES , Rohre



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