High Power Laser and Particle Beams, Volume. 36, Issue 4, 043028(2024)
Experimental study on mechanism of removing hazardous space debris based on strong electromagnetic irradiation
[2] [2] Kitamura S. Large space debris rebiter using ion beam irradiation[C]The 61st International Astronautical Federation. 2010: 725735.
[5] [5] renucci M, Pergola P, Ruggiero A, et al. Active removal of space debris exping foam application f active debris removal[R]. Affiliation: European Space Agency, Advanced Concepts Team, 2011.
[7] Elizabeth S. Spacecraft materials development programs for thermal control coatings and space environmental testing[J]. Solar Energy Mater Solar Cells, 7, 73-83(2000).
[8] Li Peng, Xiao Zejuan, Cheng Huier. Numerical model study of thermal analysis on multilayer perforated insulation material in orbit[J]. Chinese Space Science and Technology, 26, 17-20,36(2006).
[9] Zhao Yibo, Yang Ruping, Qiu Riyao, . Recent progress on multi-layer insulation structures[J]. Aerospace Materials & Technology, 43, 29-34(2013).
[10] [10] Li Yao. Study on electromagic radiation effect of thermal control layer in a vacuum[D]. Beijing: Nth China Electric Power University, 2022
[11] Yuan Guang. Theoretical progress in field electron emission[J]. Vacuum Electronics, 30-34(2012).
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Nuoci Huang, Eryan Yan, Hao Yang, Xiangyang Bao, Xingchen Liu, Hu He. Experimental study on mechanism of removing hazardous space debris based on strong electromagnetic irradiation[J]. High Power Laser and Particle Beams, 2024, 36(4): 043028
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Received: Oct. 25, 2023
Accepted: Mar. 22, 2024
Published Online: Apr. 22, 2024
The Author Email: Eryan Yan (yaneryan_2002@163.com)