The invention relates to a modular configuration suitable for small satellites launched in batches, and belongs to the field of configuration design of the small satellites. Comprising a satellite body, a front butt joint adaptive frame, two rear butt joint adaptive frames and two supporting plates. The satellite body is horizontally placed; the front docking adapter frame is mounted on the central axis of the front end of the satellite body; the two rear butt joint adaptive frames are symmetrically installed on the two side walls of the rear end of the satellite body. The front butt joint adaptive frame and the two rear butt joint adaptive frames are horizontally arranged; the front butt joint adaptive frame and the two rear butt joint adaptive frames form an isosceles triangle structure; one of the supporting plates is connected with the front butt joint adaptive frame and one of the rear butt joint adaptive frames; the other supporting plate is connected with the front butt joint adaptive frame and the other rear butt joint adaptive frame; the technical problem that a traditional small satellite configuration method is difficult to adapt to batch production and launching is solved, and the method has the capability of quickly establishing a satellite constellation system.
本发明涉及一种适用于批量发射的小卫星的模块化构型,属于小卫星的构型设计领域;包括卫星本体、前对接适配架、2个后对接适配架和2个支撑板;卫星本体水平放置;前对接适配架安装在卫星本体的前端中轴线上;2个后对接适配架对称安装在卫星本体后端的2侧壁处;前对接适配架和2个后对接适配架均水平设置;前对接适配架与2个后对接适配架组成等腰三角形结构;其中1个支撑板连接前对接适配架与其中1个后对接适配架;另1个支撑板连接前对接适配架与另1个后对接适配架;本发明解决了传统小卫星构型方法难以适应批量生产和发射的技术难题,具备快速组建卫星星座系统的能力。
Modularized configuration of small satellites suitable for batch launching
一种适用于批量发射的小卫星的模块化构型
2023-05-05
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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