제1 및 제2 대향 벽을 갖는 하우징, 및 제1 및 제2 벽에 걸쳐 있는 하우징 내부의 지지 구조를 포함하는 위성 장치가 개시된다. 지지 구조는 제1 및 제2 벽에서만 하우징에 구조적으로 연결되고, 지지 구조의 단부는 분리 시스템에 의해 발사체에 연결되도록 구성되어 있다.

    A satellite apparatus is disclosed, including a housing (234, 334) having first (236, 336) and second (238, 238) opposing walls, and a support structure (260, 360) inside the housing (234, 334) spanning the first (236, 336) and second (238, 338) walls. The support structure (260, 360) is structurally connected to the housing (234, 334) only at the first (236, 336) and second (238, 338) walls, and an end portion (262, 362) of the support structure (260, 360) is configured for connection to a launch vehicle (124) by a separation system (106, 410, 412).


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    Titel :

    STACKED SATELLITE ASSEMBLIES AND RELATED METHODS


    Weitere Titelangaben:

    적층 위성 조립체 및 관련 방법



    Erscheinungsdatum :

    24.06.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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