The invention provides a high-orbit satellite platform configuration with parallel and tiled central bearing cylinder type storage tanks. The high-orbit satellite platform configuration comprises a platform structure, a propulsion system and a solar cell array, wherein the propulsion system is mounted on the platform structure, and the solar cell array is mounted outside the platform structure and can be switched between a folded state and an extended state. According to the platform structure, an electronic cabin and a propulsion cabin are subjected to functional area division, the propulsion cabin has a complete independent physical entity, and parallel integration of the electronic cabin and the propulsion cabin can be achieved, so on one hand, welding integration of a propulsion system and testing and maintenance of a propulsion valve part assembly can be conveniently conducted through the propulsion cabin, and on the other hand, a supporting structure on an electronic cabin side is good in opening performance and large in cabin capacity, convenient conditions are created for the electronic cabin to flexibly adapt to assembling, disassembling, testing, checking and the like of on-satellite instruments and equipment, and the application requirements of high-orbit remote sensing satellites can be met.
本发明提供了一种中心承力筒式贮箱并联平铺的高轨卫星平台构型,包括平台结构、推进系统以及太阳电池阵,所述推进系统安装在所述平台结构上,所述太阳电池阵安装在所述平台结构的外部并能够在折叠状态和伸展状态之间切换,本发明平台结构内部将电子舱与推进舱进行功能区域划分,推进舱具有完整独立物理实体,能够实现电子舱与推进舱并行集成,一方面便于利用推进舱对推进系统进行焊装集成、推进阀门部组件的测试与维护,另一方面电子舱侧的支撑结构开畅性好,舱容大,为电子舱灵活适应星上仪器设备的装拆、测试和检查等创造便捷条件,可满足高轨遥感卫星的应用需求。
High-orbit satellite platform configuration with parallel and tiled central bearing cylinder type storage tanks
中心承力筒式贮箱并联平铺的高轨卫星平台构型
2021-06-18
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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