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《Spacecraft Envionment Engineering》 2002-02
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DONG Hong-jian TONG Jing-yu WANG Ji-hui SUN Gang PANG He-wei CHEN Bi-zhong HUANG Ben-cheng (Beijing Institute of Spacecraft Environment Engineering,Beijing 100029,China)  
This article introduces the feasibility test of laser-driven debris.In the test,four bonding methods are compared,and the velocity of aluminum flyer is also measured in a vacuum chamber.Moreover the damage assessment on two protective materials is performed.The results of the test show that it is necessary,and feasible to build a set of complete laser- driven debris device in the lab.
【CateGory Index】: V416;V417
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Chinese Journal Full-text Database 1 Hits
1 WU Li-zhi,SHEN Rui-qi,XU Jiao,YE Ying-hua,HU Yan(School of Chemical Engineering,Nanjing University of Science and Technology,Nanjing 210094,Jiangsu,China);Research Advance in Laser-driven Flyer Technology[J];Acta Armamentarii;2010-02
Chinese Journal Full-text Database 5 Hits
1 Chen Lang  Feng Changgen  (School Mechatronic Engineering, Beijing Institute of Technology, Beijing, 100081  ) (Laboratory for Shock Wave and Detonation Physics Research, Southwest Institute of Fluid Physics  );FREE-SURFACE VELOCITY OF METAL PARTS DRIVEN BY EXPLOSIVES MEASURED WITH VISAR INTERFEROMETER[J];Acta Armamentarii;2003-01
2 GU Zhuo wei, SUN Cheng wei,SU Xiao yong (Institute of Fluid Physics,CAEP,Mianyang 621900,Sichuan,China);Experimental Research on Impacting and Detonating Explosive by Mini Size Laser-Driven-Flyer[J];Explosion and Shock Waves;2002-01
3 GU Zhuo wei, SUN Cheng wei, LUO Li jun (Southwest institute of fluid physics, CAEP, Mianyang 621900, China);Experimental research on laser driven flyer and its application possibility in simulation of aerospace particles[J];Infrared and Laser Engineering;2002-05
4 ZHANG Wen-bing DONG Hong-jian GONG Zi-zheng TONG Jing-yu (Beijing Institute of Spacecraft Environment Engineering,Beijing 100094,China);Hypervelocity Micro-debris Launched by Laser-driven Flyer Device[J];Equipment Environmental Engineering;2007-01
5 Tong Jingyu Pang Hewei Huang Bencheng (Beijing Institute of Spacecraft Environment Engineering,Beijing 100029);A NEW METHOD OF SPACE MICRODEBRIS HYPERVELOCITY IMPACT SIMULATION[J];Spacecraft Envionment Engineering;2001-03
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