期刊文献+

电推力器流动模拟中的电子处理方法 被引量:2

Electron simulation methods of electric thruster
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摘要 分析了电子的准中性假设、玻耳兹曼分布假设、粒子模型在电推力器流动模拟中的适用性和优劣性,提出了一种新的电子处理方法——电子漂移扩散近似,采用该方法模拟了离子发动机栅极光学系统等离子体运动过程。结果表明:该方法得出的电势分布、离子相空间分布及电子数密度分布与经典的电子玻耳兹曼分布假设处理方法计算结果一致,验证了该方法可以很好地应用于电推力器栅极光学系统模拟。 The applicability,advantages and disadvantages of quasi-neutral assumption,Boltzmann distribution assumption,and particle model of electrons in the electric thruster flow simulation are analyzed.Based on the analysis,a new method: electron drift-diffusion approximation is presented,which is used to simulate the plasma movement in optical system of ion thruster,and its feasibility is verified in optical system simulation.Simulation results show the plasma potential distribution,ion phase space distribution and the electron density distribution is consistent with the results of the Boltzmann distribution assumption,and the feasibility of this new method is verified.
出处 《强激光与粒子束》 EI CAS CSCD 北大核心 2011年第7期1940-1944,共5页 High Power Laser and Particle Beams
基金 中国博士后科学基金项目(20100471633)
关键词 电推力器 粒子模拟 漂移扩散近似 栅极光学系统 electric thruster particle model drift-diffusion approximation grid optical system
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参考文献12

  • 1Roy R 1, Hasttings D E. Modeling of ion thruster plume contamination[R]. 29th Joint Propulsion Conference and Exhibit. 1993.
  • 2Wang J, Liewer P C, Karmesin S R. 3 D deformable grid electromagnetic PIC for parallel computers[R]. 35th Aerospace Sciences Meeting and Exhibit. 1997.
  • 3Fife J. The development of a flexible, usable plasma interaction modeling system[R]. 38th Joint Propulsion Conference and Exhibit. 2002.
  • 4Gatsonis N A, Yin Xuemin. Hybrid (particle fluid) modeling of pulsed plasma thruster plumes[J].Journal of Propution and Power, 2001, 17(5) :945- 958.
  • 5lain D B. Review of hall thruster plume modeling[J]. Journal of Spacecraft and Rockets, 2001, 38(3) :381 387.
  • 6Choi Y J. Modeling an anode layer hall thruster and its plume[D]. Ann Arbor: University of Michigan, 2008.
  • 7Mahalingam S. Particle based plasma simulation for an ion engine discharge chamber[D]. Dayton: Wright State University, 2007.
  • 8Peng X, Ruyten W, Friedly V, et al. Particle simulation of ion optics and grid erosion for two grid and three grid systems[J].Review of Scientific Instruments, 1994, 65(5) : 1770 -1773.
  • 9Wang J, Brinza D, Young M. Three dimensional particle simulation modeling of ion propulsion plasma environment for deep space 1[J]. Journal of Spacecraft and Rockets, 2001, 38(3) :433- 440.
  • 10Wang J, Usui H. Kinetic simulations of ion beam neutralization[R]. 31th Internationa Electric PropuLsion Conference. 2009.

同被引文献21

  • 1贺武生,孙安邦,毛根旺,霍超,陈茂林.离子推力器放电腔数值模拟[J].强激光与粒子束,2010,22(12):3020-3024. 被引量:7
  • 2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
  • 3Tighe W G, Chien K R, Solis E. Performance evaluation of the XIPS 25-cm thruster for application to NASA discovery missions[R]. AIAA 2006-4666, 2006.
  • 4Hiatt J M, Wilbur P J. Ring cusp discharge chamber performance optimization[R]. AIAA 85-2007,2007.
  • 5Kitamura S, Miyazaki K, Hayakawa Y, et al. Performance improvement of 150-raN xenon ion thrusters[J]. Acta Astronautica, 2003,52 (1):11-20.
  • 6Brophy J R, Wilbur P J. Simple performance model for ring and line cusp ion thrusters[J]. AIAA Journal, 1985,23(11) :1731-1736.
  • 7Goebel D M, Wirz R E, Katz I. Analytical ion thruster discharge performance model[R]. AIAA 2006-4486, 2006.
  • 8Goebel D M. Ion source discharge performance and stability[J]. Physics of Fluids, 1982,25(6) : 1093-1102.
  • 9Okawa Y, Takegahara H, Tachibana T. Numerical analysis of ion beam extraction phenomena in an ion thruster[C]//27th International Electric Propulsion Conference. 2001.
  • 10Goehel D M, Katz I. Fundamentals of electric propulsion: ion and Hall thruster[M]. California: JPL Space Science and Technology Series,2008 : 100-141.

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