期刊文献+

水工质脉冲等离子体推进器的能量平衡和效率 被引量:1

On the energy balance and efficiency of water-fed pulsed plasma thruster
下载PDF
导出
摘要 通过一种同轴水工质脉冲等离子体推进器的LCR放电回路的理论分析和实验来探讨其在运行过程中的能量平衡和能量转换效率。理论分析认为储能电容中的储存能量通过放电转化为加速动能及被传输线和电容的等效电阻消耗掉,并且根据等效电阻的分配情况定义了水工质脉冲等离子体推进器的加速动能和电磁力转换效率。实验研究表明:该水工质脉冲等离子体推进器的存储能量(E0=4.86J)转换成加速动能的能量转换效率是28%,其中11%用于电磁加速及17%用于电热加速,其余72%的存储能量消耗在储能电容和传输线内阻所造成的能量损失上。 The energy balance and conversion efficiency were discussed by analyzing and experimenting LCR discharging circuit of the coaxial water-fed pulsed plasma thruster.The analysis shows that storage energy in the main capacity is converted into kinetic energy and consumed by the capacity equivalent resistance.According to the allocation of equivalent resistance,the conversion efficiency of accelerator and electric magnetic forces of water-fed pulsed plasma thruster is defined.The experiment indicates that,the energy conversion efficiency that the dump energy(E0 =4.86J) of the water-fed pulsed plasma thruster is converted into accelerator is of 28%,among which 11% is used for electromagnetic acceleration and 17% for electrothermal acceleration,and that 72% of storage energy is consumed by the storage capacity and internal resistance of transmission line.
出处 《推进技术》 EI CAS CSCD 北大核心 2011年第2期292-295,300,共4页 Journal of Propulsion Technology
基金 教育部博士学科点专项科研基金(20060288005) 江苏省自然科学基金(BK2007209) 国家自然科学基金(50375050)
关键词 脉冲等离子体推进器 能量平衡 效率 水工质 等效电路 Pulsed plasma thruster Energy balance Efficiency Water-fed Equivalent circuit
  • 相关文献

参考文献2

二级参考文献8

  • 1Haag Torn W, Pencil Eric J. A performance comparison of pulsed plasma thruster electrode configurations [ C ]. 25^th International Electric Propulsion Conference Sponsored by the Electric Rocket Propulsion Society Cleveland, Ohio, August 24-28, 1997.
  • 2Rhodes R, Keefer D, Thomas H. A numerical study of a pulsed plasma thruster [ R]. AIAA 2001-3895.
  • 3Joseph R Cassady, W Andrew Hoskins. A micro pulsed plasma thruster (PPT) for the " dawgstar" spacecraft [ C ]. IEEE 2000 7803-5846-5.
  • 4Guman W J. Pulsed plasma technology in microthrusters [ R ]. Fairchild Hiller Corp, Farmingdale, NY, AFAPL- TR-68-132, Nov. 1968.
  • 5Gregory G Spanjers, Keith A, Frank S, et al, Investigation of propellant inefficiencies in a pulsed plasma thruster [R]. AIAA 96-2723.
  • 6Lynn A Arrington, Thomas W hag. Multi-axis thrust measurements of the EO-1 pulsed plasma thruster [ R] - AIAA 99-2290.
  • 7Hani Kamhawi, Eric Pencil, Thomas Haag. High thrustto-power rectangular pulsed plasma thruster [ R]. AIAA 2002-3975.
  • 8朱毅麟.电推进的现状与展望[J].上海航天,1998,15(3):48-53. 被引量:13

共引文献6

同被引文献19

  • 1Koizumi H, Kakami A, FumtaY, et al. Liquid propellant pulsed plasma thruster[C]//28~h International Electric Propulsion Conference. Toul- ouse, France: IEPC, 2003: 1-10.
  • 2Koizumi H, Kawazoe Y, Komurasaki IC Effect of solute mixing in the liquid propellant of a pulsed plasma thruster[J]. Vacuum, 2006 80(1): 11-12.
  • 3Scharlemann C A, Yoke M T. Pulsed plasma thruster using water propellant, part I: investigation of thrust behavior and mechanism[C]// 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Huntsville, USA: AIAA, 2003: 5022.
  • 4Scharlemann C A, Yoke M T. Pulsed plasma thruster using water propellant, part II: thruster operation and performance evaluation[C]// 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Huntsville, USA: AIAA, 2003: 5023.
  • 5Simon D L, Emhoff H B. Experimental evaluation of a micro liquid pulsed plasma thruster concept[C]// 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Sacramento, USA: AIAA, 2006: 4330.
  • 6Koizumi H, Kakami A, EurutaY, etal. Design and performance of liquid propellant pulsed plasma thruster [J]. Vacuum, 2004, 73(3): 419-425.
  • 7Koizumi H, Furtua ~, Komurasaki K, et aL A pulsed plasma thruster using water as the propellant[C]//40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Fort Lauderdale, USA: AIAA, 2004 3460.
  • 8Scharlemann C A, Yoke M T, Turchi P J. Alternative propellants for pulsed plasma thrusters[C] // 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Indianapolis, USA: AIAA, 2002: 4270.
  • 9Scharlemann C A. Investigation of thrust mechanisms in a water fed pulsed plasma thruster [D]. Columbus, USA: The Ohio State Univer- sit'y, 2003: 1-170.
  • 10杨乐脉冲等离r体推力器工作过程理论和实验研究[D].长沙:国防科技大学,2007:1—114.

引证文献1

二级引证文献2

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