Dynamic response of pulsed laser-irradiated space debris

Abstract

High-velocity small-sized space debris with a diameter of 1–10 cm can cause huge damage to orbiting satellites and spacecraft. In recent years, the technology of actively removing small-sized space debris by high-energy pulsed laser irradiation has attracted widespread attention from scholars around the world, who strive for giving the maximum protection to the safety of the low-earth orbit environment. This paper focuses on exploring the dynamic behavior of centimeter-sized space debris under space-based pulsed laser irradiation. For this purpose, a fluid-structure-thermal-plasma multiphysics coupling model is built for space debris, and the effect law of plasma plumes produced by space debris after laser irradiation at different time is drawn. The simulation and measurement results are compared for analysis, verifying the validity and reliability of the proposed method and the built simulation model. The findings of this study are expected to provide an important theoretical reference and guidance for the research on the application of pulsed lasers to the active removal of centimeter-sized space debris.

References

[1] DuJ L. Research on space-based monitoring system for space debris cataloging[D], 2018, Wuhan, Wuhan University: 1-7(in Chinese)

[2] LiM, GongZ Z, LiuG Q. Space debris monitoring and removal frontier technology and system development[J]. Science bulletin, 2018, 63(25):2570-2591

[3] YUTA E, HIROHISA K, PAVEL T. New formulation for evaluating status of space debris capture using tether-net[J]. Advances in space research, 2022, 70(10).

[4] WenQ, YangL W, ZhaoS H, et al.. Removing small scale space debris by using a hybrid ground and space based laser system[J]. International journal for light and electron optics, 2017, 141: 105-113

[5] TsurutaH, DondelewskiO, KatagiriY, et al.. Ablation spot area and impulse characteristics of polymers induced by burst irradiation of 1 µm laser pulses[J]. Acta astronautica, 2017, 136: 46-54

[6] KatsuhikoT, SatoshiW, TakayoO, et al.. Laser ablation induced impulse study for removal of space debris mission using small satellite[J]. Applied physics A, 2022, 128(10):932

[7] FangY W, ZhaoS H, YangL W, et al.. Study on the interaction law of small-scale space debris in low earth orbit irradiated by ground-based laser[J]. Infrared and laser engineering, 2016, 45(2): 15-20

[8] BattistonR, BurgerW J, CafagnaA, et al.. A systematic study of laser ablation for space debris mitigation[J]. The journal of space safety engineering, 2017, 4(1):36-44

[9] ChangH. Nanosecond laser ablation impulse coupling characteristics and its application in space debris removal[D], 2014, Beijing, Equipment Institute: 1-5(in Chinese)

[10] DengY, JiX L, LiX Q, et al.. Optimal momentum coupling between the ground-based laser impulse and space debris[J]. Applied physics B, 2022, 128(8):138

[11] FangY W. Space-based pulse laser removal of near-earth small debris[J]. International journal for light and electron optics, 2021, 226(1): 165898

[12] MurtazaA, PirzadaS, XuT, et al.. Orbital debris threat for space sustainability and way forward[J]. IEEE access, 2020, 8(99): 1

[13] AliM, HendaR. Modeling of plasma expansion during pulsed electron beam ablation of graphite[J]. MRS advances, 2017, 2(16): 905-911

[14] WeiY. Research on numerical simulation method of laser matter interaction based on finite element analysis[D], 2017, Jilin, Changchun University of Technology: 17-23(in Chinese)

[15] ChangH, JinX, YeJ F, et al.. Analysis of propulsive flow field characteristics of nanosecond pulsed laser ablation of typical materials in vacuum environment[J]. Propulsion technology, 2017, 38(6):1427-1433