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圆柱形Hall推力器磁场的设计与数值模拟 被引量:5

Magnetic field design and numerical simulation of cylindrical Hall thrusters
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摘要 霍尔(Hall)推力器的磁场设计是提高其性能的关键技术之一。针对传统环形Hall推力器小型化带来的缺点,提出了圆柱形的Hall推力器。简要对比了环形和圆柱形两种推力器,对圆柱形推力器的工作原理、磁场设计的要求以及利用ANSYS有限元软件进行的电磁场数值模拟的结果进行了详细分析。结果表明,圆柱形推力器磁路设计是合理的,另外也证明了用ANSYS有限元软件进行电磁场模拟的可靠性。 The magnetic field design of a Hall thruster is essential to the engine performance improvement. Cylindrical Hall thruster was proposed in this paper considering disadvantages of traditional ring-shaped Hall thruster minimization. A brief comparision was made between ring-shaped and cylindrical Hall thruster. Detailed analyses on the principles of operation, the magnetic field design requirements as well as the numerical simulation results obtained through ANSYS finite element software of the cylindrical thruster were conducted. The results indicated that this cylindrical booster magnetic circuit design is reasonable, moreover reliability of the ANSYS finite element software which was used to simulate the electromagnetic field is proved.
出处 《火箭推进》 CAS 2007年第5期32-36,共5页 Journal of Rocket Propulsion
基金 国家自然科学基金:10675040
关键词 Hall推力器 等离子体 ANSYS有限元软件 电磁场 数值模拟 Hall thruster plasma ANSYS finite element software electromagnetic field numerical simulation
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参考文献4

  • 1[1]Yevgeny Raitses,Artem Smirnov,Nathaniel J Fisch.Performance of a low-power cylindrical Hall thruster[D].Princeton University Plasma Physics Laboratory (PPPL).The 29th inter-national electric propulsion conference.2005.
  • 2[2]Edgar Y Choueiri.Fundamenta difference the two variants of Hall thrusters SPT and TAL[R].AIAA-2001-3504.
  • 3[3]Keidar M,Boyd I D.On the magnetic mirror effect in Hall thrusters[J].Applied physics letters 87,2005,12.
  • 4杨乐,李自然,尹乐,吴建军,周进.脉冲等离子体推力器研究综述[J].火箭推进,2006,32(2):32-36. 被引量:14

二级参考文献25

  • 1牛禄,王宏伟,杨威.用于微小卫星推进装置的脉冲等离子体推力器[J].上海航天,2004,21(5):39-43. 被引量:20
  • 2[2]Burton R.L.Pulsed Plasma Thruster[J].Journal of Propulsion and Power,Vol.14,No.5,1998,pp 716-735.
  • 3[3]D L Tilley.Life Extension Strategies for Space Shuttle-Deployed Small Satellites Using a Pulsed Plasma Thruster[R].AIAA 96-2730.
  • 4[4]Francis M Curran.Pulsed Plasma Thruster Technology Directions[R].AIAA 97-2926.
  • 5[6]D C MacLELLAN.Lincoln Experimental Satellites 5and 6[R].AIAA 70-0494.
  • 6[7]W J Guman.Pulsed Plasma Micro-thruster for Synchronous Meteorological Satellite (SMS)[R].AIAA73-1066.
  • 7[8]W.L.Ebert.Operation Nova Spacecraft Teflon Pulsed Plasma Thruster System[R].AIAA 89-2497.
  • 8[9]J R LeDuc.Mission Planning,Hardware Development,and Ground Testing for the Pulsed Plasma Thruster (PPT)Space Demonstration on MightySat Ⅱ[R].AIAA97-2279.
  • 9[10]Scott W.Benson.Development of a PPT for the EO-1Spacecraft[R].AIAA 99-2276.
  • 10[11]J K Ziemery.Performance Characterization of a High Efficiency Gas-Fed Pulsed Plasma Thruster[R].AIAA 97-2925.

共引文献13

同被引文献26

  • 1Deli Tang, Lisheng Wang, Shihao Pu, et al. Characteristics of end Hall ion source with magnetron hollow cathod discharge [J]. Nucl. Instrum. Meth. Phys. Res. B, 2007, 257: 796-800.
  • 2Gavrilov N V, Oks E M. High-current pulse sources of broad beams of gas and metal ions for surface treatment [J]. Nucl. Instrum. Meth. Phys. Res. A, 2000, 439: 31- 44.
  • 3Wutte D, Freedman S, Gough R, et al. Development of an rf driven multicusp ion source for nuclear science experiments [J]. Nucl. Instrum. Meth. Phys. Res. B, 1998, 142:409 -416.
  • 4Deli Tang, Jie Zhao. Effects of magnetic field gradient on ion beam current in cylindrical hall ion source [J]. Journal of Applied Physics, 2007, 102: 123305.
  • 5Richard R H, Robert S J. The influence of current density and magnetic field topography in optimizing the performance, divergence,and plasma oscillations of high specific impulse hall thrusters [R]. IEPC-2003-142.
  • 6Barral S, Makowski K, Gascon N, ets. Wall material effects in stationary plasma thrusters [ J ]. Physics of Plasmas, 2003, 10 (10).
  • 7TANG De-li, ZHAO Jie, WANG Li-sheng, PU Shi-hao, CHENG Chang-ming, Paul K. Chu, Effects of magnetic field gradient on ion beam current in cylindrical hall ion source[ J]. Journal of Applied Physics 102, 123305 (2007).
  • 8Keidar M, Boyd 1 D. On the magnetic mirror effect in Hart thrusters[ J]. Applied Physics Letters 87, 121501 (2005).
  • 9TANG De-li, WANG Li-sheng, PU Shi-hao, CHENG Changming, Paul K. Chu, Characteristics of end Hall ion source with magnetron hollow cathode discharge[ J]. Nuclear Instruments and Methods in Physics Research B, 257 (2007) 796 -800.
  • 10Morozov A I, Savel'ev V V. One-dimensional hydrodynamic model of the atom and ion dynamics in a stationary plasma thruster[ J ]. Plasma Physics Reports, 2000, 26 ( 3 ) : 219- 224.

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