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激光等离子体微推进技术的研究进展

叶继飞 洪延姬 王广宇 李南雷

中国光学2011,Vol.4Issue(4):319-326,8.
中国光学2011,Vol.4Issue(4):319-326,8.

激光等离子体微推进技术的研究进展

Research progress in micro-laser plasma propulsion

叶继飞 1洪延姬 2王广宇 1李南雷1

作者信息

  • 1. 装备指挥技术学院研究生院,北京101416
  • 2. 装备指挥技术学院基础部,北京101416
  • 折叠

摘要

Abstract

To achieve the applications of micro-Laser Plasma Propulsion(μLPP) to aerospace fields,the development of the μLPP technologies during 10 years was introduced.The different working modes for the μLPP were discussed and their advantages and disadvantages were analyzed briefly.The effects of laser micro ablation of a target on μLPP properties were also introduced,which involves the state of target,structure of target,doped target,and the liquid target.For the purpose of the micro satellite orbit and posture control,the micro-Laser Plasma Thrusters(μLPTs) developed by Phipps group in America were analyzed.Finally,the shortcomings in the research were pointed out and the further development of μLPP technology was given.

关键词

激光等离子体微推进/工作模式/靶特性

Key words

micro-laser plasma propulsion/work mode/target character

分类

信息技术与安全科学

引用本文复制引用

叶继飞,洪延姬,王广宇,李南雷..激光等离子体微推进技术的研究进展[J].中国光学,2011,4(4):319-326,8.

基金项目

国家973重点基础研究发展规划资助项目(No.61328) ()

中国光学

2095-1531

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