The invention discloses a space debris removing method and system. The method comprises the steps that a satellite platform carrying a debris removing device is controlled to move to a predetermined tiny space debris gathering orbit; and the debris removing device is controlled to emit a high-energy particle beam, high-energy particles in the high-energy particle beam are attached to a tiny spacedebris surface, and a charge quantity of the tiny space debris surface is increased so that the tiny space debris falls into the atmosphere of the earth after reducing a running orbit. Effective removal of the tiny space debris of a near-earth orbit can be realized.
本申请公开了一种空间碎片清除方法与系统,该方法包括:控制搭载有碎片清除装置的卫星平台运动至预先确定的微小空间碎片聚集轨道;控制碎片清除装置发射高能粒子束,高能粒子束中的高能粒子附着于微小空间碎片表面,增大微小空间碎片表面的电荷量,以使微小空间碎片降低运行轨道后坠入地球大气层。可以实现对近地轨道微小空间碎片的有效清除。
Space debris removing method and system
空间碎片清除方法与系统
2020-09-15
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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