期刊文献+

离子推力器电子反流的理论预测与试验测量 被引量:2

THEORY AND EXPERIMENT OF BACK-STREAMING FOR ION THRUSTER
在线阅读 下载PDF
导出
摘要 对离子推力器来说,加速栅的作用是提供一个负的电势壁垒,阻止下游的电子反流到放电室内部。反流电子流不仅会导致推力器能量损失,严重的甚至会导致推力器无法工作。电子反流阈值是由加速栅孔内的鞍点电势所决定的,而决定鞍点电势的因素有屏栅和加速栅的电势,屏栅和加速栅的几何结构,子离子束流的大小。推导了鞍点电热公式,采用监测屏栅电流的变化的方法,测量出反流阈值,并与理论计算值相比较。 For ion thruster,the accel grid can produce a potential barrier to stop neutralizer electrons from flowing back into the discharge chamber. The backstreaming electron current is not only a parasitic power loss , but it can damage the thruster. The back-streaming limit is determined by the "saddle-point" voltage and the factors related to the "saddle-point" including the vohage of screen grid and accelerator grid ; the structure of grids ; the beamlet current. In general, there are two methods to measure the back-streaming limit. This paper choose the method to monitor the increase in the screen power supply current as the magnitude of the accelerator grid vohage is decreased.
出处 《真空与低温》 2013年第2期105-109,99,共6页 Vacuum and Cryogenics
关键词 电推进 电子反流 鞍点电势 ion thruster back-streaming saddle-point voltage
  • 相关文献

参考文献6

  • 1贾艳辉,李忠明,张天平,李小平,陈继巍,陈娟娟.栅极系统电子返流对离子推力器寿命影响[J].真空与低温,2012,18(1):21-25. 被引量:3
  • 2John D. Williams,Dan M. Geobel ,Paul J. Wilbur. Analytical Model of Electron Baekstreaming rIonThmsters[C]. AIAA,2003- 4560.
  • 3John Steven Snyder, John R. Brophy. Performance Characterization and Vibration Testing of30-cm Caron-Carbon Ion Optics[C]. AIAA,2004-3959.
  • 4Richard E. Wirz, Ira Katz, Dan M. Goebel, et al. Electron Backstreaming Determination for Ion Thrusters [ J ]. AIAA,2008-4732.
  • 5John E. Foster,Robert F. Roman,George C. Soulas, et al. Electron Backstreaming Mitigation via a Magnetic Grid[ R]. IEPC-01- 91.
  • 6Brian T. Young, Jacques C. Richand. Lattice Boltzmann Models of Xe, Xe , Xe++, e- Flow through Ion Thruster Optics [ C ]. AIAA, 2006-5006.

二级参考文献16

  • 1张天平.国外离子和霍尔电推进技术最新进展[J].真空与低温,2006,12(4):187-193. 被引量:66
  • 2BROPHY J R, KAKUDA R Y, POLK J E, et al. Ion Propulsion System DS1 Technology Validation Report[R]. DS1 technology validation report, 2000-10.
  • 3BROPHY J R, POLK J E, RANDOLPH T M, et al. Lifetime Qualification of Electric Thrusters for Deep-Space Missions [ R]. AIAA-2008-5184.
  • 4BROPHY J R, POLK J E, PLESS L C. Test to Failure of a Two Grid Ion Accelerator System[ R]. IEPC-1993-172.
  • 5JONATHAN L, NOORD V. Lifetime Assessment of The NEXT Ion Thruster[ R I. AIAA-2007-5274.
  • 6POLK J E, MOORE N R, NEWLIN L E, et al. Probabilistic Analysis of Ion Engine Accelerator Grid Life[ R]. IEPC-1993-176.
  • 7WILLIANMS J D, GOEBELL D M, WILBUR P J. Analytical Nodel of Electron Backstreaming for Ion Thruster[ R]. AIAA-2003- 4560.
  • 8POLK J E, MOORE N R, BROPHY J R, et al. The Role of Analysis and Testing in The Service Life Assessment of Ion Engine [ R ]. IEPC-1995-228.
  • 9BROPHY J R, KATZ I, PLOK J E, et al. Numerical Simulations of Ion Thruster Accelerator Grid Erosion [ R ]. AIAA-2002- 4261.
  • 10ANDERSON J R, KATZ I, GOEBEL D. Numerical Simulation of Two-grid Ion Optics Using a 3D Code [ R]. AIAA-2004-3782.

共引文献2

同被引文献35

  • 1张天平.国外离子和霍尔电推进技术最新进展[J].真空与低温,2006,12(4):187-193. 被引量:66
  • 2Patterson M J,Haag T W,Rawlin V K,et al. NASA 30 cm ionthruster development status[C]//Presented at the 30th JointPropulsionConference,Indianapolis,IN,1994:27-29.
  • 3Patterson M J,Haag T W,Hovan S A. Performance of theNASA 30 cm Ion Thruster[C]//AIAA,DGLR,AIDAA,andJSASS,IEPC,23rd,Seattle,WA,1993.
  • 4WallaceNC,FeamDG,CoplestonRE.Thedesignandperfor.manceoftheT6ionthruster[J].AIAAPaper,1998:98-3342.
  • 5Wallace N C,Mundy D H,Fearn D G,et al. Evaluation of thePerformance of the T6 Ion Thruster[C]//35th Joint PropulsionConference,1999.
  • 6Snyder J,Goebel D M,Hofer R R,et al. Performance evalua.tion of the T6 ion engine[J]. Journal of Propulsion and Power,2012,28(2):371-379.
  • 7Tighe W G,Chien K R,Solis E,et al. Performance evaluationof the XIPS 25-cm thruster for application to NASA discoverymissions[R].AIAA,2006.
  • 8TigheWG,Kuei-RuC,etal.UpdateontheXIPS8-cmThrust.erPrototype[R].AIAA,2008-4912.
  • 9Polk J E,Kakuda R Y,Anderson J R,et al. Performance of theNSTAR ion propulsion system on the Deep Space One mission[R].AIAA,2001,965.
  • 10PattersonMJ,BensonSW.NEXTionpropulsionsystemdevel.opment status and performance[M]. National Aeronautics andSpaceAdministration,GlennResearchCenter,2008.

引证文献2

二级引证文献6

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