期刊文献+

微波等离子推力器真空实验研究 被引量:3

Experimental investigation of microwave plasma thruster in vacuum
下载PDF
导出
摘要 微波等离子推力器(MPT)具有寿命长、效率高和比冲高的特点,具有广泛的应用前景。通过对MPT真空实验系统,以及中(~1kW)、低(~100W)功率MPT结构的介绍,重点论述了MPT在真空环境下的启动和稳定工作特性,并对实验结果进行了分析和讨论,给出了MPT初步性能参数。实验结果表明,在30W~1kW功率范围内,MPT真空环境下启动可靠,工作稳定;氦气(He)的比冲远高于氩气(Ar)的比冲。 Microwave Plasma Thruster (MPT) is a new type of electrothermal thruster. Its characteristics include light weight, long lifetime, high efficiency and high specific impulse. Both types of MPT 100 W and 1 kW incident power at frequency of 2.45 GHz and vacuum experimental system are introduced. The characteristics of MPT under vacuum condition are emphatically described. Results of experiment demonstrate that they can reliably start up and steadily operate from 30 W to 1 kW incident power under vacuum condition. The specific impulse of helium (He) propellants is higher than that of Argon (Ar).
出处 《推进技术》 EI CAS CSCD 北大核心 2003年第3期208-211,共4页 Journal of Propulsion Technology
基金 国家"八六三"基金 (863 2 2 1 2 ) 国防基础科研项目(J1 40 0D0 0 1 ) 西北工业大学博士论文创新基金资助项目
关键词 微波等离子推力器 谐振器 圆柱体 同轴谐振腔 真空试验 Cavity resonators Electric propulsion Microwaves Plasma devices Vacuum
  • 相关文献

参考文献2

二级参考文献8

共引文献50

同被引文献14

  • 1毛根旺,韩先伟,杨涓,黄晓砥,何洪庆.微波电热推力器启动与稳定过程的实验观测[J].宇航学报,2000,21(z1):84-88. 被引量:5
  • 2朱国强.水工质MPT推进机理研究及关键部件设计.西北工业大学硕士论文.西安:西北工业大学,2008:3-6.
  • 3Brandenburg J E, Kline J, Sullivan D. The microwave electro-ther- mal(MET) thruster using water vapor propellant. IEEE Transactions on Plasma Science, 2005; 33(2) :776-780.
  • 4阎超.计算流体力学方法及应用.北京:北京航空航天大学出版社,2007.
  • 5Brandenburg J E, Zooghby M E I. Progress on the MET ( Microwave Electro-Thermal) thruster using water propellant. AIAA 2006- 5179, 2006.
  • 6Power J L, Sullivan D J. Preliminary investigation of high power microwave plasma for electrothermal thruster use[R]. AIAA 93-2106.
  • 7Diamant J E, Brandenburg. Performance measurement of a water fed microwave electrothermal thruster [ R]. AIAA 2001-3900.
  • 8Souliez F J, Chianese S G, Dizac G H, et al. Low-power microwave arcjet testing: plasma and plume diagnostic and performance evaluation [ C ] . Ch. 7 in Micropropulsion for Small Spacecraft, Progress in Astronautics and Aeronautics, Vol. 187,AIAA, Restron
  • 9Yang Juan, He Hongqing, Mao Genwang, et al. Resonant and ground experimental study on microwave plasma thruster [ J ].Journal of Spacecraft and Rockets, 2003,40(4).
  • 10[美]Shari Lawrence Pfleeger著,Software Engineering Theory and Practice.

引证文献3

二级引证文献10

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