본 발명은 지상에서 우주궤도 또는 우주공간까지 탑재물을 운송하기 위한 우주발사체에 관한 것으로, 더욱 상세하게는 우주발사체의 동체와 동체 내부에 수용되는 추진제 탱크를 탄소섬유 강화 복합재를 이용하여 제작하는 탄소복합재 초경량 우주발사체 동체 및 그 제조 방법에 관한 것이다.

    The present invention relates to a space launch vehicle for transporting a load from the earth to a space orbit or to space and, more specifically, to a carbon composite ultralight space launch vehicle fuselage manufactured using a carbon fiber reinforced composite for the fuselage of the launch vehicle and a propellant tank accommodated in the fuselage, and a manufacturing method thereof.


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    Titel :

    Lightweight Space Launch Vehicle Fuselage Structure and Design Method of the Same


    Weitere Titelangaben:

    초경량 우주발사체 동체 및 그 제조 방법


    Beteiligte:
    HWANG DAEHYUN (Autor:in) / YOUK SANGWOO (Autor:in) / SHIN DONGYOON (Autor:in)

    Erscheinungsdatum :

    10.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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