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Mechanism and operation parameters of a plasma-driven micro-particle accelerator
Authors:Huang  JianGuo  Han  JianWei  Li  HongWei  Cai  MingHui  Li  XiaoYin  Zhang  ZhenLong  Chen  ZhaoFeng  Wang  Long  Yang  XuanZong  Feng  ChunHua
Institution:(1) Center for Space Science and Applied Research, Chinese Academy of Sciences, P.O. Box 8701, Beijing, 100190, China;(2) Institute of Physics, Chinese Academy of Sciences, P.O. Box 603, Beijing, 100190, China
Abstract:There is a large amount of micro debris ranging between millimeters and micrometers in space, which has significant influence on the reliability and life of spacecrafts through long-duration integrated impacts and has to be considered in designing a vehicle’s suitability to the space environment. In order to simulate the micro-impacts on exposed materials, a plasma-driven micro-particle accelerator was developed. The major processes, including the acceleration, compression and ejection of plasmas, were modeled. By comparing the theoretical simulations with the experimental results, the acceleration mechanism was clarified. Moreover, through a series of experiments, the optimum operation range was investigated, and the acceleration ability was primarily determined. Supported by the Project of Development and Transformation of Scientific Equipment from Chinese Academy of Sciences (Grant No. Y2003011)
Keywords:plasma  space debris  hypervelocity impact  experimental simulation
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