The invention relates to the technical field of aerospace, in particular to an array type multi-satellite satellite-rocket separation device which comprises satellites, a locking separation unit, a connecting rod mechanism, a pressing unit, a rotary pressure regulating unit and a satellite-rocket docking platform. The plurality of rotary voltage regulating units are fixed on the satellite-rocket docking platform, and the rotary voltage regulating units are arranged in two rows; the lower end of one connecting rod mechanism is hinged with one row of rotary pressure regulating units, and the lower end of the other connecting rod mechanism is hinged with the other row of rotary pressure regulating units; a plurality of satellites are stacked on the satellite-rocket docking platform, the two connecting rod mechanisms are connected together through the locking and separating units to form an integral frame, and the satellites are wrapped; the multiple pressing units are connected to the connecting rod mechanism, and the pressing units can be adjusted up and down so that the lower end faces of the pressing units can be pressed on the upper surface of the satellite on the uppermost layer. Satellite-rocket connection interfaces can be reduced, the design difficulty is reduced, the space utilization rate is improved, the number of carried satellites is increased, and space junk is reduced.
本申请涉及航空航天技术领域,尤其涉及一种阵列式多星星箭分离装置,包括:卫星、锁紧分离单元、连杆机构、压紧单元、回转调压单元和星箭对接平台;多个回转调压单元固定至星箭对接平台上,并且所述回转调压单元排列成两排;一个连杆机构的下端与一排回转调压单元铰接,另一个连杆机构的下端与另一排回转调压单元铰接;多个卫星叠放在星箭对接平台上,多个锁紧分离单元将两个连杆机构连接在一起,组成一个的整体的框架,将所述卫星包裹起来;多个压紧单元连接在连杆机构上,且压紧单元可上下调节使其下端面压紧在最上层的卫星的上表面上。本申请可以减少星箭连接接口,降低设计难度,提高空间利用率,增加搭载卫星的数量,并且减少太空垃圾。
Array type multi-satellite-rocket separating device and satellite-rocket locking and separating method
一种阵列式多星星箭分离装置及星箭锁紧、分离方法
2024-06-25
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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