The trap has a propellant gas serving as a conveying medium, and an arrangement for separation of the gas from a liquid fuel. Guide plates are provided in a rotationally symmetrical collecting container and are arranged radially in a region of an outer wall e.g. half-spherical shell (3), cylindrical shell (4) and conical shell (5), of the container. A gas separator tapers conically toward an outlet pipe (2) of the container and includes passage holes. Screens are arranged between the separator and the pipe. The separator and the screens are arranged close to an outlet region of the container.


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    Titel :

    Blasenfalle für Treibstofftanks in Raumflugkörpern


    Weitere Titelangaben:

    Bubble trap for propellant tanks in spacecraft
    Piège à bulles pour réservoir d'ergol dans des engins spatiaux


    Beteiligte:

    Erscheinungsdatum :

    13.06.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Deutsch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke