The invention provides a satellite cabin, a spaceflight satellite and a satellite cabin manufacturing method, and relates to the technical field of spaceflight satellites. The satellite cabin comprises a cabin plate, a plug connector, a flexible circuit board and a controller. The plug connector, the flexible circuit board and the controller are all pre-buried in the cabin plate. The plug connector is in communication connection with the flexible circuit board. And the flexible circuit board is in communication connection with the controller. The plug connector is used for being electrically plugged with a single machine. The satellite cabin is low in structural design and assembly difficulty, high in assembly efficiency, clean and tidy in cabin, large in operable space in cabin and low in satellite research and development and launching cost.

    本申请提供一种卫星舱、航天卫星和卫星舱制造方法,涉及航天卫星技术领域。卫星舱包括舱板、插接件、柔性电路板和控制器。插接件、柔性电路板和控制器均预埋于舱板。插接件与柔性电路板通信连接。柔性电路板与控制器通信连接。插接件用于与单机电插接。该卫星舱的结构设计,装配难度低,装配效率高,舱内整洁,舱内可操作空间大,卫星研发和发射成本低。


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    Titel :

    Satellite cabin, space satellite and satellite cabin manufacturing method


    Weitere Titelangaben:

    卫星舱、航天卫星和卫星舱制造方法


    Beteiligte:
    HU LIHONG (Autor:in) / FENG MINGPENG (Autor:in) / GUO TAO (Autor:in) / ZHENG PING (Autor:in) / ZHAO HONGJIE (Autor:in) / LU CHUAN (Autor:in)

    Erscheinungsdatum :

    29.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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