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arXiv · 2608.17245

Assessing Collision Probability in Low-Thrust Deorbit

Shuta Fukii·Daisuke Sakai·Yasuhiro Yoshimura·Yuri Matsushita·Toshiya Hanada·Yuki Itaya·Tadanori Fukushima
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Abstract

End-of-life support of satellites is necessary to improve post-mission-disposal compliance rates for maintaining space environment. Deorbit mission with low thrust, e.g. a laser, induces a low-level deceleration on the target object that gradually lowers the target altitude. Since such a low-thrust trajectory is time-consuming, the risk of collision greatly influences the mission success rate. In this context, this paper assesses the collision risk during deorbit trajectories with low thrust. Furthermore, parametric studies for the relationship between the re-entry time and the risk of collision are performed.

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Shuta Fukii, Daisuke Sakai, Yasuhiro Yoshimura, Yuri Matsushita, Toshiya Hanada, Yuki Itaya, Tadanori Fukushima. 2026-08-18. Assessing Collision Probability in Low-Thrust Deorbit. https://arxiv.org/abs/2608.17245

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