The invention relates to a satellite batch launching system based on a stacking mode, and relates to the technical field of satellites, the satellite batch launching system comprises a mounting seat pressing rod and a plurality of satellites, and the satellites are stacked on a mounting seat; a positioning assembly is arranged between every two adjacent satellites, each positioning assembly comprises a positioning column and a sleeve, the positioning columns are fixedly arranged on the bottom walls of the satellites, and the sleeves are fixedly arranged on the top walls of the satellites and used for allowing the positioning columns to be inserted so as to limit the positions of the two adjacent satellites. A first elastic piece for driving the positioning column to be separated from the sleeve is arranged in the sleeve; the pressing rod is hinged to the mounting base, and a pressing assembly used for applying pressing force to a satellite is arranged on the pressing rod. When the satellites are separated, the pressing assembly is unlocked, the satellite on the upper layer is pushed under the action of the first elastic piece, the positioning column is made to be separated from the sleeve, and at the moment, the satellite on the upper layer can be unlocked and separated.
本申请涉及一种基于堆叠方式的卫星批量发射系统,涉及卫星技术领域,包括安装座压杆和多个卫星,多个所述卫星堆叠设置在安装座上;相邻两卫星之间设置有定位组件,所述定位组件包括定位柱和套筒,所述定位柱固定设置于卫星的底壁,所述套筒固定设置于卫星的顶壁,用于供定位柱插入以限定相邻两卫星的位置,所述套筒内设置有用于驱使定位柱脱离套筒的第一弹性件;所述压杆铰接于安装座上,所述压杆上设置有用于对卫星施加压紧力的压紧组件。卫星分离时,压紧组件进行解锁,在第一弹性件的作用下上层的卫星被推动并使得定位柱脱离套管,此时上层的卫星即可实现解锁分离。
Satellite batch launching system based on stacking mode
一种基于堆叠方式的卫星批量发射系统
12.01.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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