The present invention relates to a satellite loading device and a satellite operation method. According to the present invention, the satellite loading device comprises: a main body part having a storage space to store a plurality of satellites; a mounting part installed inside the main body part to enable the satellite to be detachably restrained; and a support unit capable of detachably restraining another satellite to the satellite. The plurality of satellites can be mounted, launched, and ejected from a single mounting device.

    본 발명은 인공위성 탑재 장치 및 인공위성 운용 방법에 관한 것으로, 복수의 인공위성을 수납할 수 있도록 수납공간을 가지는 본체부; 인공위성을 분리 가능하게 구속시킬 수 있도록, 상기 본체부의 내부에 설치되는 탑재부; 및 상기 인공위성에 다른 인공위성을 분리 가능하도록 구속시킬 수 있는 지지부;를 포함하고, 하나의 탑재 장치에 복수의 인공위성을 탑재하여 발사하고, 사출시킬 수 있다.


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    Titel :

    Satellite mounting device and method for operating satellite


    Weitere Titelangaben:

    인공위성 탑재 장치 및 인공위성 운용 방법


    Beteiligte:
    KIM DONG YEON (Autor:in)

    Erscheinungsdatum :

    14.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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