期刊文献+

微型电推力器的研究与发展 被引量:3

Research and Development of Micro Electric Thruster
在线阅读 下载PDF
导出
摘要 随着微型卫星技术的迅猛发展,为了满足微型卫星各种飞行姿态变化的任务要求,兼具功能性和高可靠性的微推进技术,特别是微型电推进技术已经成为微型卫星发展的迫切需求。近年来,自由分子流微电热推力器、射频电容耦合放电微推力器、微射频离子推力器、微腔放电推力器、场致发射电推力器、微胶体推力器和微波激励微等离子体推力器等微型电推力器研究势头良好,已完成工程样机研制,有望于若干年内实现空间应用。 With the rapid development of micro satellite technology, the micro propulsion with high perform-ance and high reliability is needed urgently, especially micro-electric propulsion technologies. Nearly years, a number of micro-electric propulsion technologies have been developed, such as free molecular micro-resistojet( FM-MR), radio frequency capacitive coupling discharge micro-thruster, micro cavity discharge thruster( MCDT), mi-cro radio Frequency Ion Thruster( RIT), Field Emission Electric Thruster( FEET), micro-colloid thruster and mi- crowave excited micro-plasma thruster. The engineering prototypes have been developed for these micro propulsion technologies, and its will be available for space application in several years.
出处 《科学技术与工程》 北大核心 2012年第16期3924-3932,共9页 Science Technology and Engineering
关键词 电推力器 微推进 微型电推进 等离子体推进 electric thruster micro propulsion miniature electric propulsion plasma propulsion
  • 相关文献

参考文献81

  • 1Ahmed Z , Gimelshein S F, Ketsdever A. Numerical analysis of free- molecule micro-resistojet performance. Journal of Propulsion and Power,2006 ;22(4) :749 -756.
  • 2Ketsdever A, Green A, Muntz E P, et al. Fabrication and testing of the free molecule micro-resistojet : initial Results. Collection of Tech- nical Papers -- 36rd AIAA/ASME/SAE/ASEE Joint Propulsion Con- ference, 2000:3672.
  • 3Lee R H, Bauer A M, Killingsworth M D, et al. Performance charac- terization of the free molecule micro-resistojet utilizing water propel- lant. Collection of Technical Papers -- 43rd AIAA/ASME/SAE/AS- EE Joint Propulsion Conference, 2007:1748--1758.
  • 4韩先伟,唐周强,陶文铨,张贵田,张恩昭.自由分子流微电热推力器工作特性和性能研究[J].固体火箭技术,2005,28(2):83-86. 被引量:4
  • 5Lee R H, Lilly T C, Muntz E P, et al. Free molecule micro-resisto- jet :nanosatellite propulsion. Collection of Technical Papers -- 41rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2005--4073.
  • 6陈茂林,毛根旺,杨涓,夏广庆.自由分子流微电热推力器(FMMR)流动模拟与喷嘴型面分析[J].固体火箭技术,2008,31(2):107-110. 被引量:1
  • 7张晰哲,韩先伟,陈祖奎,等.基于水推进剂的自由分子流微型电阻加热推进系统.第十四届全国等离子体科学技术会议暨第五届中国电推进技术学术研讨会会议摘要集,中国大连,2009:125.
  • 8蒋建,管海兵.用于FMMR微推进系统的微型自锁阀.第十四届全国等离子体科学技术会议暨第五届中国电推进技术学术研讨会会议摘要集,中国大连,2009:132.
  • 9栾希亭,张晰哲,韩先伟,陈祖奎,毛根旺.FMMR微推进系统推力测量装置研究[J].固体火箭技术,2011,34(4):525-528. 被引量:5
  • 10Rutledge T S, Micci M M, Bilen S G. Design and Initial tests of a Low power radio-frequency electrothermal thruster. 44th Joint Pro- pulsion Conference and Exhibit, Hartford, 2008---4537.

二级参考文献62

共引文献45

同被引文献29

  • 1曾海蓉,李婷娜,冉倩,王琳,任媛媛,彭伟,高永翔,黄勤挽,谭瑾.基于熵权法结合Box-Behnken响应面法优化桂枝芍药知母颗粒复方提取工艺[J].中草药,2020,51(1):84-90. 被引量:72
  • 2尤政,张高飞,任大海.MEMS微推进技术的研究[J].纳米技术与精密工程,2004,2(2):98-105. 被引量:20
  • 3王永菲,王成国.响应面法的理论与应用[J].中央民族大学学报(自然科学版),2005,14(3):236-240. 被引量:639
  • 4余伟元,顾佐,李娟.对离子光学系统数值模拟算法的分析[J].科学技术与工程,2006,6(21):3467-3469. 被引量:1
  • 5WOLF E T. Porous emitter colloid thruster performancecharacterization using optical techniques, ADA582612[R].2013.
  • 6GAMERO-CASTA O M,HRUBY V. Electrosprayas asource of nanoparticles for efficient colloidthrusters[J]. Journal of Propulsion and Power,2001,17(5) : 977-987.
  • 7GAMER()-CASTA O M. Characterization of a six-emittercolloid thruster using a torsional balance [j]. Journal ofPropulsion and Power, 2004, 20(2): 736-741.
  • 8SONG W, SHUMLAK U. Ultrasonically aidedelectrospray source for charged particle approachingmonodisperse distributions [J]. Journal of Propulsionand Power, 2010,26(2) : 353-363.
  • 9SONG W, SHUMLAK U. Charged nanoparticle sourcefor high thrust level colloid thruster [J]. Journal ofPropulsion and Power, 2008,24(1): 146-148.
  • 10DONG L, SONG W, KANG X M, et aL A performance comparison of ultrasonically aided electric propulsion extractor configurations[J]. Acta Astronautica, 2012, 77: 1-11.

引证文献3

二级引证文献7

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部