The embodiment of the invention discloses a folding type flat plate satellite configuration which comprises a main body flat plate platform. A load bearing flat plate platform is annularly distributed on the edge of the main body flat plate platform; A rotary unfolding mechanism is positioned between the main body flat plate platform and the load bearing flat plate platform; A rotary unfolding mechanism is configured to enable the load bearing flat plate platform to be unfolded and kept stable at an angle of 0-360 degrees relative to the main body flat plate platform. Each load bearing flat plate platform of the satellite configuration can carry one or more complete load systems, the load systems between the adjacent load bearing flat plate platforms are mutually independent, and batch production can be achieved; Meanwhile, the load bearing flat plate platform further has high universality and can be suitable for multiple satellite models, and the satellite research and development period can be shortened. According to the satellite configuration provided by the embodiment of the invention, integrated, universal, batch and modular design and production of satellites can be realized.
本发明实施例公开了一种折叠式平板卫星构型,包括:主体平板平台;环向分布于所述主体平板平台边缘的载荷承载平板平台;位于所述主体平板平台与所述载荷承载平板平台之间的旋转展开机构;所述旋转展开机构被配置为使得所述载荷承载平板平台相对于所述主体平板平台以0°‑360°角度展开并保持稳定。本卫星构型的每个载荷承载平板平台可搭载一套或多套完整的载荷系统,且相邻载荷承载平板平台之间的载荷系统相互独立,可以实现批量式生产;同时载荷承载平板平台还具有较强的通用性,可适用于多个卫星型号,可缩短卫星研发周期。本发明实施例所提供的卫星构型可实现卫星的集成化、通用化、批量化、模块化设计和生产。
Folding type flat plate satellite configuration
一种折叠式平板卫星构型
2021-05-28
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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