A tethered plate satellite as a sweeper of small space debris

被引:14
|
作者
Takeichi, Noboru [1 ]
Tachibana, Naoki [1 ]
机构
[1] Tokyo Metropolitan Univ, Dept Aeronaut & Astronaut, 6-6 Asahigaoka, Tokyo 1910065, Japan
关键词
Space debris removal; Tethered system; Orbital manoeuvre; Collision; Re-entry; AVOIDANCE MANEUVERS; REMOVAL; STRATEGY; CAPTURE; ORBIT; DYNAMICS; SYSTEM; NETS;
D O I
10.1016/j.actaastro.2021.08.051
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Removing space debris is an urgent task to ensure sustainable space activity. Towards this end, we propose herein a tethered plate satellite that can remove many items of small space debris successively by collisions alone without capturing them or performing major orbital manoeuvres. The strategy involves a tethered plate that moves more slowly than the space debris at the same altitude so that the speed difference in the collision causes re-entry of the space debris. Numerical verification using an on-orbit object database indicates that, for the requisite number of collisions, this strategy would require a reasonable amount of orbital manoeuvres. The results indicate that six such spacecraft operating for one decade would suffice to reduce the amount of removable space debris in a certain altitude range by 96.10%. Based on these results, a mission concept is proposed in which debris-removal systems would remove almost all the removable space debris in a given altitude range, thereby allowing for the operation of large satellite constellations.
引用
收藏
页码:429 / 436
页数:8
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