The invention discloses a rotary throwing separation method and system for stacked panel satellites. The system comprises a rocket last-stage rocket body, a flat satellite, stacked satellite locking devices and stacked satellite guiding force bearing columns, the tail end of the rocket last-stage rocket body is connected with a satellite adapter, the satellite adapter is connected with the multiple stacked satellite locking devices, the flat satellite is wrapped in an area defined by the multiple stacked satellite locking devices, and the stacked satellite guiding force bearing columns are connected with the flat satellite. The flat plate satellite is locked through the stacked satellite locking device, and when the stacked satellite locking device is loosened, the flat plate satellite is separated from the stacked satellite locking device; a plurality of rows of flat satellites are stacked in parallel in the flat satellites, the flat satellites in each row are mutually nested and guided through the stacked satellite guiding bearing columns, and the flat satellites in each row are detachably connected. According to the method, stacking and rotary throwing separation of the flat satellites can be achieved, the satellites do not collide with one another in the rotary throwing separation process, the near-field separation safety of the stacked satellites is greatly improved, and the safety of the satellites is protected.
本发明公开一种堆叠平板卫星旋抛分离方法及系统。所述系统包括火箭末级箭体、平板卫星、堆叠卫星锁紧装置和堆叠卫星导向承力柱,火箭末级箭体的末端连接卫星适配器,在卫星适配器连接多个堆叠卫星锁紧装置,平板卫星包裹在多个堆叠卫星锁紧装置围成的区域内,并通过堆叠卫星锁紧装置锁定平板卫星,堆叠卫星锁紧装置松开时,平板卫星脱离堆叠卫星锁紧装置;平板卫星中平行堆叠排布多排平板卫星,每排平板卫星之间通过堆叠卫星导向承力柱相互嵌套和导向,每排平板卫星之间可分离连接。本方法可实现平板卫星堆叠和旋抛分离,并且卫星在旋抛分离过程彼此互不相碰,大大提升了堆叠卫星的近场分离安全性,保护了卫星的安全。
Stacked panel satellite rotary throwing separation method and system
一种堆叠平板卫星旋抛分离方法及系统
2023-07-18
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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