The invention provides a load multi-point installation satellite configuration, which comprises a satellite main structure, a solar cell array, a multi-point installation load unit and platform equipment, and is characterized in that the satellite main structure comprises a bottom plate, a layer plate, a top plate and side plates, the number of the side plates is at least three, and the side plates are connected end to end to define a main body frame; the bottom plate is installed at the bottom of the main body frame, the top plate is installed at the top of the main body frame, the layer plate is installed in the middle of the main body frame, the solar cell array comprises a cell substrate, and the cell substrate is installed on the outer side face of the side plate. The invention further provides a rapid assembly method of the satellite configuration with the load installed at the multiple points. The invention has the beneficial effects that the whole configuration is designed around the load, a multi-point non-coplanar structure and thermal control integrated installation design thought is given by optimizing the layout of equipment in the cabin, and the installation precision is ensured while the heat dissipation of the load is effectively solved.
本发明提供了一种载荷多点安装的卫星构型,包括卫星主结构、太阳电池阵、多点安装载荷单元和平台设备,其中,所述卫星主结构包括底板、层板、顶板以及侧板,所述侧板至少有三个并首尾连接围合形成主体框架,所述底板安装在主体框架的底部,所述顶板安装在主体框架的顶部,所述层板安装在所述主体框架的中部,所述太阳电池阵包括电池基板,所述电池基板安装在所述侧板的外侧面。本发明还提供了一种载荷多点安装的卫星构型的快速装配方法。本发明的有益效果是:整个构型围绕载荷设计,通过优化舱内设备布局给出了一种多点不共面,结构与热控一体化安装设计的思路,有效解决了载荷的散热同时保证了安装精度。
Load multi-point installation satellite configuration and rapid assembly method
一种载荷多点安装的卫星构型及快速装配方法
2022-12-20
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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