The invention relates to the field of satellite mechanisms, in particular to a satellite deorbit device. The satellite deorbit device comprises a bottom plate, side cover plates, a power source assembly, a driven assembly, a sail truss mechanism and a locking mechanism, the peripheral area of the bottom plate is rotationally connected with the side cover plates, the power source assembly and the driven assembly in transmission connection with the power source assembly are arranged in the central area, the driven assembly is in sliding connection with one end of the locking mechanism, and the other end of the locking mechanism is connected with the side cover plates in a clamped mode; a containing space is formed by the bottom plate and the side cover plates, a sail unfolding film capable of being unfolded is arranged in the containing space, the corners of the sail unfolding film are fixedly connected with the extending end of the sail truss mechanism, and the sail truss mechanism is connected with the driven assembly and driven by the driven assembly to extend out. According to the satellite deorbit device, the power source assembly can be controlled through the control signal, and the sail unfolding process of the satellite deorbit device is controlled; the unfolding success rate of the deorbit sail is improved, and the satellite hang time is shortened.
本申请涉及卫星机构领域,特别涉及一种卫星离轨装置;卫星离轨装置包括底板、侧盖板、动力源组件、从动组件、帆桁机构和锁紧机构,底板的四周区域和多个侧盖板转动连接,其中中央区域设有动力源组件及与其传动相连的从动组件,从动组件与锁紧机构的一端滑动连接,另一端与侧盖板卡接;底板和多个侧盖板构成容置空间,容置空间内设有可张开的展帆薄膜,展帆薄膜的边角与帆桁机构的伸出端固定连接,帆桁机构与从动组件相连并由其驱动伸出;本申请的卫星离轨装置能够通过控制信号控制动力源组件,控制卫星离轨装置的展帆进程;提高离轨帆的展开成功率,减少卫星滞空时间。
Satellite deorbit device
一种卫星离轨装置
2022-04-01
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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