Paper
19 October 2016 The shape effect of space debris on recoil impulse by pulsed laser ablation
Chenglin Wang, Yan Zhang, Kunpeng Wang
Author Affiliations +
Proceedings Volume 10152, High Power Lasers, High Energy Lasers, and Silicon-based Photonic Integration; 101520E (2016) https://doi.org/10.1117/12.2245326
Event: International Symposium on Optoelectronic Technology and Application 2016, 2016, Beijing, China
Abstract
Removing space debris by high-energy pulsed laser may be the most effective way to mitigate the threat posed by the increasing space debris. Laser ablation of a thin surface layer causes recoil impulse, which will lower the orbit perigee of space debris and accelerate the atmospheric capture. When the laser beam vertically irradiates a flat debris, it requires a certain laser fluence to reach the optimal impulse coupling, and the recoil impulse is parallel to the laser beam. However, the incident laser fluence varies in different parts of a non-flat surface. We have taken the shape effect into account to propose a numerical method of calculating the recoil impulse. Taking cylinder debris as the target, we have compared the recoil impulse in different laser fluences through simulation experiments, which implies that a higher laser fluence than the optimal one is needed to obtain a larger recoil impulse for irregularly shaped space debris.
© (2016) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Chenglin Wang, Yan Zhang, and Kunpeng Wang "The shape effect of space debris on recoil impulse by pulsed laser ablation", Proc. SPIE 10152, High Power Lasers, High Energy Lasers, and Silicon-based Photonic Integration, 101520E (19 October 2016); https://doi.org/10.1117/12.2245326
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