The invention relates to the technical field of spaceflight, in particular to a flat plate type satellite configuration. The flat plate type satellite configuration comprises a first mounting plate, a second mounting plate opposite to the first mounting plate and a frame clamped between the first mounting plate and the second mounting plate, and the first mounting plate and the second mounting plate are arranged on the two opposite sides of the frame; the frame comprises a plurality of edge beams connected end to end and a plurality of middle beams detachably fixed to the inner sides of the edge beams, and the interior of the frame is divided into a plurality of containing spaces used for containing satellite single machines through the middle beams. According to the flat plate type satellite configuration, the frame is clamped between the first mounting plate and the second mounting plate, the bearing capacity can be improved, the manufacturing difficulty and cost are reduced through detachable connection of the middle beams and the edge beams, and protection can be provided for the satellite single machine through the containing space.

    本发明涉及航天技术领域,特别是涉及一种平板式卫星构型。本发明的平板式卫星构型,包括第一安装板、与第一安装板相对设置的第二安装板、以及夹设于第一安装板和第二安装板之间的框架,第一安装板和第二安装板设于框架的两个相对侧;框架包括首尾相连的若干边梁、以及可拆卸地固定至边梁内侧的若干中间梁,若干中间梁将框架的内部分隔为多个用于容纳卫星单机的容纳空间。本发明的平板式卫星构型通过框架夹设于第一安装板和第二安装板之间,可以提升承载能力,通过中间梁与边梁可拆卸地连接,降低制造难度及成本,通过容纳空间能够为卫星单机提供防护。


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    Title :

    Flat plate type satellite configuration


    Additional title:

    一种平板式卫星构型


    Contributors:

    Publication date :

    2025-03-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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