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《Equipment Environmental Engineering》 2007-01
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Hypervelocity Micro-debris Launched by Laser-driven Flyer Device

ZHANG Wen-bing DONG Hong-jian GONG Zi-zheng TONG Jing-yu (Beijing Institute of Spacecraft Environment Engineering,Beijing 100094,China)  
laser-driven flyer device is one of the important ground systems to simulate hypervelocity impact of space debris to spacecraft.Velocity and integrity of the flyer are the key parameters for the device.The effects on the velocity and integrity of flyer in- duced by laser parameters,substrate and ablation layer of flyer targets were discussed.Thickness design and rang of material selection for the substrate and ablation layer of flyer target were also discussed.In recent study,7μm thickness,1 mm diameter aluminum flyer can be launched to 8.3km/s,and the structure of flyer target is single-layered.
【CateGory Index】: V528
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【References】
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
【Citations】
Chinese Journal Full-text Database 1 Hits
1 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
【Co-citations】
Chinese Journal Full-text Database 6 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
2 ZHANG Wenbing ( Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China );Velocity Measurement Technologies of Space Debris Driven by Ground-base Simulation Devices[J];Spacecraft Environment Engineering;2006-03
3 HAN Jianwei, ZHANG Zhenlong, HUANG Jian’guo, LI Xiaoyin, CHEN Zhaofeng, QUAN Ronghui, LI Hongwei ( Center for Space Science and Applied Research, Beijing 100080, China );Launching of Hypervelocity Micro Space Debris by Plasma Accelerator[J];Spacecraft Environment Engineering;2006-04
4 Zhang Wenbing Gong Zizheng Dong Hongjian Yang Jiyun Tong Jingyu Xiang Shuhong (Beijing Institute of Spacecraft Environment Engineering,Beijing 100094,China);Parameter analysis of laser-driven flyer technique[J];Spacecraft Environment Engineering;2007-03
5 Jia Zhexin Gong Ke He Shufang Huo Yujing (Department of Electronic Engineering,Tsinghua University,Beijing 100084,China);High-Speed Flyer Velocity Measurement System Based on Laser Scattering[J];Chinese Journal of Lasers;2008-07
6 ZHAO Xing-hai,GAO Yang,ZHAO Xiang (Institute of Electronic Engineering,China Academy of Engineering Physics,Mianyang 621900, China);Development of laser initiation technology[J];Infrared and Laser Engineering;2009-05
【Co-references】
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 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
5 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);FEASIBILITY TEST OF LASER-DRIVEN DEBRIS[J];Spacecraft Envionment Engineering;2002-02
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