Chinese Journal of Lasers, Volume. 39, Issue s1, 102015(2012)
Research of Micro Laser Thruster Engine Performance Based on Thermodynamic Cycle Analysis
[1] [1] Ye Jifei, Hong Yanji, Wang Guangyu. Progress of research in laser micro ablation of target[J]. Journal of Propulsion Technology, 2009, 30(6): 751~756
[2] [2] Nan Baojiang, Zhang Gangchui, Wu Ping et al.. Analysis of energy conversion efficiency of solid propellant for laser ablative propulsion[J]. Journal of Propulsion Technology, 2007, 28(5): 478~480
[3] [3] Hong Yanji, Li Xiuqian, Wang Diankai et al.. Some recommendations on condensed propellants for laser propulsion[J]. Journal of Propulsion Technology, 2009, 30(5): 618~624
[4] [4] Hong Xin, Zhang Baojiong. Basic of Rocket Engine[M]. Beijing: Science Press, 2003. 33~34
[5] [5] Sun Chengwei. Laser Irradiation Effect[M]. Beijing: National Defense Industry Press, 2002. 86~113
[6] [6] Ye Jifei, Hong Yanji, Wang Guangyu et al.. Effects of target character on propulsion performance in laser micro propulsion[J]. Acta Optica Sinica, 2011, 31(s): s100521
[8] [8] Ye Jifei, Wang Guangyu, Wang Diankai. Measurement of laser ablation micro impulse using the torsion pendulum interferometry[C]. The 2nd International Conference on Advanced Measurement and Test, 2011, Advanced Materials Research Vols. 301-303: 1078~1082
[9] [9] Ye Jifei, Hong Yanji, Wang Guangyu et al.. Measurement method of microgram amounts laser ablation mass[J]. Journal of Propulsion Technology, 2010, 31(3): 372~376
[10] [10] Claude R. Phipps, James R. Luke, Wesley Helgeson et al.. 3 ks specific impulse with a ns-pulse laser microthruster[C]. International Electric Propulsion Conference, 2005. 319~323
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Ye Jifei, Hong Yanji, Wang Guangyu, Wang Diankai. Research of Micro Laser Thruster Engine Performance Based on Thermodynamic Cycle Analysis[J]. Chinese Journal of Lasers, 2012, 39(s1): 102015
Category: Laser physics
Received: Oct. 30, 2011
Accepted: --
Published Online: May. 28, 2012
The Author Email: Jifei Ye (yjf1981@163.com)