等离子体微推进技术的研究进展 -

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等离子体微推进技术的研究进展

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

基金项目:

国家973重点基础研究发展规划资助项目(No.61328)

详细信息

作者简介:
叶继飞(1981-),男,吉林辽源人,硕士研究生,讲师,主要从事微推进技术方面的研究。 E-mail:yjf1981@163.com

中图分类号:TN249; V448.2
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- 被引次数:0
出版历程
- 收稿日期:2011-05-12
- 修回日期:2011-07-23
- 刊出日期:2011-08-25

Research progress in micro-laser plasma propulsion

1.
Company of Postgraduate Management,Academy of Equipment Command&Technology,Beijing 101416,China;
2.
Deptartment of Basic Theories,Academy of Equipment Command&Technology,Beijing 101416,China

摘要

摘要:为了加快等离子体微推进技术(LPP)在航天领域的应用,介绍了该项技术近10年的发展状况。讨论了等离子体微推进技术发展过程中衍生出的各种工作模式,并简略分析了不同工作模式的优缺点。着重介绍了靶特性对微推进性能的影响,包括靶材的选择、靶的结构、靶材掺杂,以及靶物相特性等。针对该项技术的最终发展目标是研制微小卫星姿轨控的等离子体微推力器( LPT),介绍并分析了美国Phipps小组开展的微推力器的研制工作。最后,指出了等离子体微推进技术目前存在的一些问题,并展望了它的发展前景。
- 等离子体微推进/
- 工作模式/
- 靶特性
Abstract:To achieve the applications of micro-Laser Plasma Propulsion(LPP) to aerospace fields, the development of the LPP technologies during 10 years was introduced. The different working modes for the LPP were discussed and their advantages and disadvantages were analyzed briefly. The effects of laser micro ablation of a target on LPP 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(LPTs) developed by Phipps group in America were analyzed. Finally, the shortcomings in the research were pointed out and the further development of LPP technology was given.
- micro-laser plasma propulsion/
- work mode/
- target character

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参考文献 (1)

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