An electrical umbilical system for a space launch vehicle, using an electromagnet comprises: a connection module which is provided to a launch vehicle unit flyable by means of thrust; and an umbilical unit which is provided to a tower unit supporting the launch vehicle unit so as to stand upright, and which may be electrically connected to the connection module. The umbilical unit comprises: a supply module which may be electrically connected to the connection module; a connection drive module which is coupled to the tower unit and connects the supply module to the connection module; a weight body which is coupled to the tower unit so as to be vertically movable; a drive line which connects the supply module and the weight body; and a guide roller which is rotatably coupled to the tower unit and supports the drive line.


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    Titel :

    ELECTRICAL UMBILICAL SYSTEM FOR SPACE LAUNCH VEHICLE, USING ELECTROMAGNET


    Weitere Titelangaben:

    ELEKTRISCHES VERSORGUNGSSYSTEM FÜR RAUMSTARTFAHRZEUG MIT ELEKTROMAGNET
    SYSTÈME OMBILICAL ÉLECTRIQUE POUR VÉHICULE LANCEUR SPATIAL, UTILISANT UN ÉLECTROAIMANT


    Beteiligte:
    LEE JEONG CHAN (Autor:in) / MOON KEUN HWAN (Autor:in) / CHOI JONG HWI (Autor:in) / CHOI GO EUN (Autor:in)

    Erscheinungsdatum :

    02.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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