期刊文献+

基于镓铯对比的场发射电推力器分析与研制 被引量:7

Analysis and Development of Ga-FEEP Based on Comparison of Gallium and Cesium
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摘要 为解决场发射电推力器由于液态金属推进剂导致的工程化问题,分析并提出以金属镓替代现有推进剂铯的技术方案。基于推进剂镓铯物性对比,分析其对推力与比冲、发射尖端升温、热蒸发、氧化污染等的影响,论证了金属镓的工程化优势及缺点。通过研制金属镓场发射电推力器原理样机,探索并实现了液态金属镓在大气环境中的加注与润湿,在点火试验中获得准线性场发射形貌,表明金属镓是场发射推力器的良好推进剂替代物。 A technical proposal of using metal Ga instead of Cs was designed to solve the engineering prob-lems of Field Emission Electric Propulsion (FEEP) caused by liquid metal propellant. On the basis of the com-parison of physical property between Ga and Cs,the effects on the thrust,efficiency,specific impulse,emit-ter tip warming,thermal evaporation,oxidation and pollution were listed to indicate the pros and cons of Ga. By developing the principle prototype of Ga-FEEP,liquid metal Ga was successfully filled and wetted under air con-dition. Quasi-linear field emission was observed in ignition experiments. The results indicate that Ga is a good propellant substitution of FEEP.
出处 《推进技术》 EI CAS CSCD 北大核心 2015年第2期314-320,共7页 Journal of Propulsion Technology
基金 中国科学院知识创新工程“空间先进重力测量”项目
关键词 场发射电推力器 润湿 FEEP Cesium Gallium Wetting
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  • 1毛根旺,韩先伟,杨涓,何洪庆.电推进研究的技术状态和发展前景[J].推进技术,2000,21(5):1-5. 被引量:49
  • 2张郁.电推进技术的研究应用现状及其发展趋势[J].火箭推进,2005,31(2):27-36. 被引量:43
  • 3Paita L, Cesari U, Nania F, et al. Alta FT-150: The Thruster for LISA Pathfinder and LISA,rNGO Missions [ C]. Paris: 9th LISA Symposium, 2013: 245-249.
  • 4Funaki I, Nakayama Y, Horisawa H. Micro- thruster Options for the Japanese Space Gravitational Wave Ob- servatory Missions [ R]. IEPC 2011-308.
  • 5TAYLOR G. Disintegration of Water Drops in Electric Field[J]. Proceedings of the Royal Society of London Se- ries A-Mathematical and Physical Sciences, 1964, 280 ( 1380): 383-397.
  • 6Andrenucci M, Marcuccio S, Genovese A. The Use of FEEP Systems for Micronewton Thrust Level Missions [R]. AIAA 93-2390.
  • 7Seharlemann C, Buldrini N, Killinger R, et al. Qualifei- ation Test Series of the Indium Needle FEEP Micro-Pro- Pulsion System for LISA Pathfinder[J]. Acta Astronauti- cs, 2011,69(2011 ) : 822-832.
  • 8Mitterauer J. Indium-An Alternative Propellant for FEEP-Thrusters[ R]. AIAA 2001-3792.
  • 9Genovese A, Marcuccio S, Andrenucci M. Experimental Behavior of FEEP Emitters Fed by a Caesium Chromate Tank[R]. AlAA 94-3243.
  • 10Rudenauer G, Fehringer M, Steiger W. Indium Field Emission Microthrusters [C]. Noordwijk: 2th European Spacecraft Proptdsion Conference, 1997.

二级参考文献21

  • 1马向国,顾文琪.聚焦离子束加工技术及其应用[J].微纳电子技术,2005,42(12):575-577. 被引量:9
  • 2许兴胜,熊志刚,金爱子,陈弘达,张道中.聚焦离子束研制半导体材料光子晶体[J].物理学报,2007,56(2):916-921. 被引量:8
  • 3Fu Q, Bryan N K A. Investigation of hybrid microlens integration with vertical-cavity surface-emitting lasers for free-space optical links [ J ] . Optics Express, 2002, 10 (9) :413-418.
  • 4Dai H J, Hafner J H, Rinzler A G, ct al. Nanotubes as nanoprobes in scanning probe microscopy[J]. Nature, 1996,384: 147-151.
  • 5Fang F Z,Xu Z W,Dong S,et al. High aspect ratio nanometrology using carbon nanotube probes in atomic force microscopy [J]. Annals of the CIRP, 2007,56. 533-536.
  • 6Dai H J, Franklin N.Exploiting the properties of carbon nanotubes for nanolithography [J]. Appl Phys Lett, 1998,73 : 1508-1510.
  • 7Akita S, Nakayama Y. Length adjustment of carbon nanotube probe by electron bombardment[J].Jpn J Appl Phys, 2002,41 : 4887-4889.
  • 8Tseng A A. Recent developments in nanofabrication using focused ion beams [J ] . Small, 2005, 1 : 924-939.
  • 9Picard Y N, Adams D P, Vasile M J.Focused ion beamshaped microtools for ultra-precision machining of cylindrical components [J]. Precision Engineering, 2003, 27 : 59-69.
  • 10[1]John W Dunning, et al. An overview of electric propulsion at NASA [R]. AIAA 2004-3328.

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