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激光等离子体微推力器的发展及热点问题
引用本文:崔村燕,洪延姬,陈景鹏,王军,何国强.激光等离子体微推力器的发展及热点问题[J].固体火箭技术,2006,29(6):427-431.
作者姓名:崔村燕  洪延姬  陈景鹏  王军  何国强
作者单位:西北工业大学航天学院,西安,710072;装备指挥技术学院,北京,101416
基金项目:国家“973”项目,新世纪优秀人才支持计划资助
摘    要:激光微推力器在航天器的轨道调整、引力补偿、位置保持、轨道机动和姿态控制等方面存在巨大的潜在优势。对近年来激光等离子体微推力器的研究和发展进行了较全面介绍,并详述了激光等离子体微推力器发展过程中的几个热点问题,包括激光等离子体微推力器的工作模式和工质的选择、推力单元结构设计、微型激光器和微推力测试方法的研究与发展现状。通过对比分析,给出了目前所研究的激光等离子体微推力器的优缺点,为国内研制激光等离子体微推力器提供了一些有益参考。

关 键 词:激光等离子体微推力器  工作模式  工质  激光器
文章编号:1006-2793(2006)06-0427-05
收稿时间:2005-11-14
修稿时间:2006-03-29

Development and key problems of laser plasma micro-thruster
CUI Cun-yan,HONG Yan-ji,CHEN Jing-peng,WANG Jun,HE Guo-qiang.Development and key problems of laser plasma micro-thruster[J].Journal of Solid Rocket Technology,2006,29(6):427-431.
Authors:CUI Cun-yan  HONG Yan-ji  CHEN Jing-peng  WANG Jun  HE Guo-qiang
Abstract:The laser plasma micro-thruster has many potential advantages in orbit adjustment,gravitation compensation,position maintenance,orbit maneuver and attitude control.Research and development on laser plasma micro-thruster in recent years were reviewed,and some key problems were introduced in detail,such as selection of working mode and medium,structure design of thrust unit,development of micro-laser and measurement method of micro-thrust.Through contrast analysis,the advantages and disadvantages of current laser micro-thruster were presented,which can provide useful reference to research and development of the laser plasma micro-thruster.
Keywords:laser plasma micro-thruster  working mode  working medium  laser
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