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P70霍尔推力器新型缓冲腔磁路对预电离及放电的影响 被引量:3

Effects of a new buffer magnetic circuit on preionization and discharge in a P70 Hall thruster
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摘要 为有效利用从P70霍尔推力器放电通道进入缓冲腔的快电子能量,考虑两个磁场特征以提高缓冲腔预电离率。一是提高磁感应强度,二是缓冲腔内从气体分配器到放电通道方向的负梯度。采用FEMM有限元磁场计算软件,在不改变推力器电离和加速通道内优化磁场特征的前提下,设计的新型缓冲腔磁路满足上述磁场特征。放电实验结果表明,在新型缓冲腔磁路下放电电流低频振荡幅值更小。新型磁路有助于延长推力器寿命,有助于电离和加速通道内电离与加速区的分离。 To recycle fast electron energy from discharge channel into buffer chamber in a P70 Hall thruster,the characteristics of magnetic field were considered to improve the preionization ratio in the buffer chamber.The first characteristic is the higher magnetic flux density.The second characteristic is the negative gradient from gas distributor to discharge channel.The new magnetic circuit is designed by FEMM magnetic field calculation software.The magnetic field of new magnetic circuit satisfied the above characteristics on the premise of not changing the optimized magnetic field in the ionization and acceleration channel.Experimental results indicate that the amplitude of discharge current low frequency oscillation is smaller.The new magnetic circuit is helpful for prolonging the thruster lifetime and improving separation of ionization zone as well as the acceleration zone in discharge channel.
出处 《推进技术》 EI CAS CSCD 北大核心 2011年第6期823-827,共5页 Journal of Propulsion Technology
基金 国家自然科学基金(51007014 50877018) 黑龙江省教育厅科学技术研究项目(12511138)
关键词 霍尔推力器 磁路 缓冲腔 预电离 Hall thruster Magnetic circuit Buffer chamber Preionization
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参考文献22

  • 1Morozov A I. The conceptual development of stationary plasma thrusters [ J]. Plasma Physics Reports, 2003, 23 ( 3 ) : 235-250.
  • 2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
  • 3Bugrova A I, Lipatov A S, Kharchevnikov V K, et al. SPT-ATON tests at kurchatov institute stands ~ R]. 1EPC 1995 -067.
  • 4Bechu S, Gascon N, Roche S, et al. Comparison be- tween two kinds of Hall thrusters: SPT100 and ATON [ RJ. A1AA 2000-3524.
  • 5Morozov A I, Bugrova A thruster plasma accelerator I, Desyatskov A V. ATON- [ J]. Plasma Physics Reports, 1997,23 (7) ~ 587-597.
  • 6Bishaev A M, Bugrova A I, Desyatskov AV. Spectral characteristics of SPT-ATON plasma radiation [ C ]. USA t Proc. 3rd International Conference on Spacecraft Propul1 sion , 2000:887-880.
  • 7Yu D R, Wei L Q, Zhao Z Y. Effect of preionization in aton-type Hall thruster on low frequency oscillation [ J]. Physics of Plasmas, 2008, 15 (2).
  • 8Yoshikawa K, Toku H, Ueda M,et al. Hall accelerator with preionization discharge [ P]. United States Patent: 4703222,2001.
  • 9Morozov A I, Bugrova A I, Desiatskov A D,et al. Re- search on two-stage engine SPT-MAG [R]. 1EPC 2003 -290.
  • 10Bugrova A I, Desyatskov A V, Kharchevnikov V K,et al.Investigation of physical processes in SPT MAG[ R ]. IEPC 2005-146.

二级参考文献7

  • 1[1]БеланНВ, КимВП.Стационарныеплазменныедвигатели(in Russian)[M].Харьковскийавиационныйинститут, 1989.
  • 2[2]Qarmain S,Martinez Sanchez M. Issues regarding the cenera-tion of and end-to-end hall thruster computational model[R].AIAA-98-3796.
  • 3[3]Belikov M. Experimental research of low-power SPT with themodified accelerating channel[R].AIAA-3786.
  • 4[4]Fructman A. Modeling the hall thruster[R].AIAA-98-3500.
  • 5[5]File J,Marinez Sanchez M. Analyzing electron-wall interactionand dynamic response in hall thrusters[R].AIAA-98-3501.
  • 6毛根旺,何洪庆.前景诱人的新型航天动力装置──微波电热推进器(MET)[J].推进技术,1997,18(3):114-116. 被引量:4
  • 7杨涓,何洪庆,毛根旺,史韶莉.微波等离子推力器微波模式的合理选择[J].推进技术,1999,20(1):76-79. 被引量:7

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同被引文献31

  • 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:61
  • 2DIAMANT K D, POLLARD J E, RAITSES Y,etal. Ionization, plume properties,and performance ofcylindrical Hall thrusters [ J ]. IEEE Trans. PlasmaSci. , 2010,38(4): 1052-1057.
  • 3HAGELAAR G J M, BAREILLES J, GARRIGUES L,et al. Two dimensional model of a stationary plasmathruster[J]. J. Appl. Phys. ’ 2002,91(9) : 5592-5598.
  • 4HOFER R R, JANKOVSKY R S, GALLIMORE AD. High-specific impulse Hall thrusters. Part 2 :efficiency analysis [J]. Journal of Propulsion andPower, 2006,22(4): 732-740.
  • 5EAGLE W E, BOYD 1 D,TREPP S G, et al. Theerosion prediction impact on current Hall thruster modeldevelopment, AIAA-2008-5087[R]. Reston: AIAA, 2008.
  • 6PEROT C, GASCON N, BONHOMME G. Signalprocessing and non-linear behavior of a stationaryplasma thruster: first results, AIAA-1999-2427[R],Reston: AIAA, 1999.
  • 7B()EUF J P, GARRIGUES L. Ij^w frequency oscillationsin a stationary plasma thruster [J]. Journal of AppliedPhysics, 1998,84(7): 3541-3554.
  • 8MOROZOV A I, BUGROVA A 1,DESYATSKOVA V? et al. ATON thruster plasma accelerator[J].Plasma Physics Reports, 1997, 23(7) : 587-597.
  • 9BARRAL S. Theoretical study of the breathingmode in Hall thrusters [C] // Proceedings of 42ndAIAA Joint Propulsion Conference, 2006 ; 5172.
  • 10BARRAL S, PERADZYHSKI Z. Ionization oscillationsin Hall accelerators[j]. Physics of Plasmas, 2010,17(1); 014505.

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