The invention provides a universal satellite configuration suitable for various loads. The universal satellite configuration comprises a platform cabin, a universal thermal control information structure plate and a satellite load, the platform cabin is provided with a universal thermal control information structural plate, and the satellite load is connected to the universal thermal control information structural plate; pre-embedded holes, pre-embedded buses and thermal control assemblies which are used for adapting to different types of satellite loads are arranged on the universal thermal control information structural plate. The flexible design idea is adopted, different load function modules can be selected and matched according to actual needs, the same satellite platform cabin can be met by configuring the universal thermal control information structural plate, adaptation to different loads is achieved, and batch production of the platform cabin is facilitated.

    本发明提供了一种适用于多类载荷的通用化卫星构型,包括:平台舱、通用化热控信息结构板以及卫星载荷;所述平台舱上设置通用化热控信息结构板,所述卫星载荷连接在所述通用化热控信息结构板上;所述通用化热控信息结构板上布置有用于适配不同类型卫星载荷的预埋孔、预埋总线以及热控组件。本申请采用柔性化设计思路可根据实际需要选配不同载荷功能模块,通过配置通用化热控信息结构板能够满足同一卫星平台舱,实现对不同载荷的适配,有利于平台舱批量生产。


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    Title :

    Universal satellite configuration suitable for various loads


    Additional title:

    适用于多类载荷的通用化卫星构型


    Contributors:
    GENG ZHIQING (author) / WANG BO (author) / LU XI (author) / DUAN XIAOWEN (author) / ZHAO LIN (author) / CHEN XIAO (author) / ZHOU LU (author) / HUANG FAN (author) / ZHANG XUGUANG (author) / WANG WEI (author)

    Publication date :

    2025-03-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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