航天器环境工程2007，Vol.24Issue(3)：148-151,4.
激光驱动飞片系统模拟空间碎片超高速撞击
The laser-driven flyer system for space debris hypervelocity impact simulations
摘要
Abstract
The laser-driven flyer system with a single pulses from a Q-switched Nd glas laser of 15 ns duration and up to 20 J energy designed to launch the aluminum films of 5 μm in thickness up to 8.3 km/s velocity, which was developed in Beijing Institute of Spacecrafts Environment Engineering(BISEE), is briefly introduced. Some experiments on the space debris hypervelocity impacts on the outer surfaces of functional materials, such as thermal control material, window glass, and OSR etc., are reviewed. The laser-driven flyer technique is shown to be promising in simulating micro M/OD hypervelocity impacting effects.关键词
空间碎片/激光驱动飞片系统/超高速撞击Key words
space debris/the laser-driven flyer system/hypervelocity impact分类
航空航天引用本文复制引用
张文兵,龚自正,杨继运,童靖宇,向树红..激光驱动飞片系统模拟空间碎片超高速撞击[J].航天器环境工程,2007,24(3):148-151,4.基金项目
空间碎片专项(KJSP06209,KJSP06210) （KJSP06209,KJSP06210）
