The invention relates to a satellite platform configuration, in particular to a flattened satellite platform with high load bearing capacity. The satellite platform comprises a plurality of platform units, connecting pieces and a separation mechanism. Wherein the platform units are arranged in a positive and negative stacking mode, the adjacent platform units arranged in the positive and negativestacking mode are connected through the connecting pieces, and each connecting piece is provided with a separation mechanism used for releasing and separating the platform units one by one. Due to theadoption of the flattened satellite platform, the flattening platform units are adopted, the problem of alternate series connection installation of fairing column sections is fully considered, and high-density stacking alternate installation is supported. A point type spring separation mechanism is adopted to support one-by-one release and separation from top to bottom. A box plate type structurewith an embedded frame is adopted in a split mode, the structural weight is reduced, and the satellite bearing capacity is improved; the modular micro satellite platform adopts a modular structure, so that interfaces of all subsystems on a satellite are simplified, and the production period is shortened.

    本发明涉及一种卫星平台构型,具体地,涉及一种扁平化高载荷承载能力卫星平台。所述卫星平台包括:若干平台单元,连接件和分离机构;其中,若干所述平台单元正反堆叠设置,正反堆叠设置的相邻所述平台单元之间通过所述连接件连接,每个所述连接上均设有分离机构,用于将平台单元以此逐个释放分离。由于采用上述技术方案,本发明采用扁平化平台单元充分考虑整流罩柱段交替串联安装问题,支持高密度堆叠交替安装。采用点式弹簧分离机构支持从上至下逐个释放分离。分体式采用内嵌框架的箱板式构型,减轻了结构重量,提升了卫星承载能力;该模块化微型卫星平台构型采用模块化构型,简化了星上各分系统接口,缩短了生产周期。


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    Title :

    Flattened satellite platform with high load bearing capacity


    Additional title:

    一种扁平化高载荷承载能力卫星平台


    Contributors:
    LONG YE (author)

    Publication date :

    2021-02-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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