通道等离子体环境对稳态等离子体推进器壁面腐蚀的影响
Effect of Tunnel Plasma Environment on Wall Erosion of Stationary Plasma Thruster
DOI: 10.12677/MET.2017.65040, PDF,    科研立项经费支持
作者: 操慧珺：厦门城市职业学院，机械与自动化工程系，福建 厦门；张志昊：厦门大学，材料学院，福建 厦门
关键词: 壁面腐蚀；预电离；电荷交换碰撞；稳态等离子体推进器；Wall Erosion； Preionization； Charge-Exchange Collision； Stationary Plasma Thruster
摘要: 稳态等离子体推进器工作过程中通道的等离子体环境参数会影响高能粒子束的分布，进而影响离子对壁面溅射的情况。本文就加入预电离腔及考虑电荷交换碰撞对壁面腐蚀的影响进行了研究。通过调整模型中预电离率参数，研究了预电离率大小对通道物理特性分布及对通道壁面常规腐蚀的影响。结果表明预电离不会影响通道内主要物理特性，但由预电离引入的额外等离子体会加剧壁面的常规腐蚀。通过加入蒙特卡洛碰撞模块得到了电荷交换碰撞对通道各项物理参数分布和壁面常规腐蚀的影响。结果表明当考虑电荷交换碰撞后，通道内高能离子密度减少，壁面常规腐蚀情况有所减缓。
Abstract: The tunnel plasma environment can affect the distribution of high energy ion beam, and then the sputter-induced wall erosion. In this paper, the effects of preionization on the physical characteristic distributions and the wall erosion are investigated. The results indicate that the preionization do not affect the main physical characteristic in the discharge channel. While the wall erosion will be aggravated by the extra sputter plasma which is introduced by the preionization process. The effects of charge-exchange collision on the physical characteristic distributions and the wall erosion are also investigated. The results show that the ion density decreases and the wall erosion alleviates after taking the charge-exchange collision into consideration.
文章引用：操慧珺, 张志昊. 通道等离子体环境对稳态等离子体推进器壁面腐蚀的影响[J]. 机械工程与技术, 2017, 6(5): 337-347. https://doi.org/10.12677/MET.2017.65040

参考文献

[1] Cao, H., Li, Q., Shan, K., et al. (2015) Effect of Preionization on the Erosion of the Discharge Channel Wall in a Hall Thruster Using a Kinetic Simulation. IEEE Transactions on Plasma Science, 43, 130-140. [Google Scholar] [CrossRef] 
[2] 扈延林, 毛威, 李栋, 等. 面向全电推进卫星的霍尔推进技术[J]. 空间控制技术与应用, 2017, 43(1): 73-78.
[3] Goebel, D.M. and Katz, I. (2008) Fundamentals of Electric Propulsion: Ion and Hall Thrusters. John Wiley & Sons Inc. Publication, New Jersey, 325-443. [Google Scholar] [CrossRef] 
[4] 钱中, 康小录, 王平阳, 等. 霍尔推力器等离子体羽流粒子模拟[J]. 上海航天, 2009, 26(4): 43-46.
[5] 康小录, 杭观荣, 朱智春. 霍尔电推进技术的发展与应用[J]. 火箭推进, 2017, 43(1):8-17.
[6] 吴汉基, 蒋远大, 张志远. 电推进技术的应用与发展趋势[J]. 推进技术, 2003, 24(5): 385-392.
[7] 毛根旺, 唐金兰. 航天器推进系统及其应用[M]. 西安: 西北工业大学出版社, 2009: 262-291.
[8] 李世忠, 陈虹. 现代小卫星技术与数字地球[J]. 遥感信息, 2000(4): 47-49.
[9] Martinez-Sanchez, M. and Pollard, J.E. (1998) Spacecraft Electric Propulsion—An Overview. Journal of Propulsion and Power, 14, 688-699. [Google Scholar] [CrossRef] 
[10] Fife, J.M., Martinez-Sanchez, M. and Szabo, J. (1996) A Numerical Study of Low-frequency Discharge Oscillations in Hall Thruster. 33th AIAA/SAE/ASME/ASEE Joint Propulsion Conference and Exhibit, AIAA-1997-3052, Seattle, Washington.
[11] Furukawa, T., Miyasaka, T. and Fujiwara, T. (2005) Control of Low-Frequency Oscillation in a Hall Thruster. Transactions of the Japan Society for Aeronautical and Space Sciences, 44, 164-170. [Google Scholar] [CrossRef] 
[12] Tamida, T., Nakagawa, T., Suga, I., et al. (2007) Determining Parameter Sets for Low-Frequency-Oscillation-Free Operation of Hall Thruster. Journal of Applied Physics, 102, 043304-1-043304-6. [Google Scholar] [CrossRef] 
[13] Barral, S. and Ahedo Galilea, E. (2009) Low-Frequency Model of Breathing Oscillations in Hall Discharges. Physical Review E, 79, 046401-1-046401-11. [Google Scholar] [CrossRef] 
[14] Yu, D.R., Wei, L.Q., Zhao, Z.Y., et al. (2008) Effect of Preionization in Aton-Type Hall Thruster on Low Frequency Oscillation. Physics of Plasmas, 15, 043502-1-043502-6.
[15] 韩轲, 魏立秋, 纪延超. P70霍尔推力器新型缓冲腔磁路对预电离及放电的影响[J]. 推进技术, 2011, 32(6): 823-827.
[16] Morozov, A.I., Bugrova, A.I. and Desyatskov, A.V. (1997) ATON-Thruster Plasma Accelerator. Plasma Physics Reports, 23, 587-597.
[17] Yu, D.R., Wang, C.S., Wei, L.Q., et al. (2008) Stabilizing of Low Frequency Oscillation in Hall Thrusters. Physics of Plasmas, 15, Article ID: 113503.
[18] Szabo, J.J. (2001) Fully Kinetic Numerical Modeling of a Plasma Thruster. Thesis for the Degree of Doctor of Philosophy, Massachusetts Institute of Technology, Cambridge, 79-126.
[19] Parra, F.I., Ahedo, E., Fite, J.M., et al. (2006) A Two-Dimensional Hybrid Model of the Hall Thruster Discharge. Journal of Applied Physics, 100, Article ID: 023304. [Google Scholar] [CrossRef] 
[20] Sommier, E., Scharfe, M.K., Gascon, N., et al. (2007) Simulating Plasma-Induced Hall Thruster Wall Erosion with a Two-Dimensional Hybrid Model. IEEE Transactions on Plasma Science, 35, 1379-1387. [Google Scholar] [CrossRef] 
[21] 刘辉, 吴勃英, 鄂鹏, 等. ATON型Hall推力器缓冲区预电离问题研究[J]. 物理学报, 2010, 59(10): 7203-7207.
[22] Vahedi, V. and Surendra, M. (1995) A Monte Carlo Collision Model for the Particle-in-Cell Method: Applications to Argon and Oxygen Discharges. Computer Physics Communications, 87, 179-198. [Google Scholar] [CrossRef] 
[23] Kafafy, R.I. (2005) Immersed Finite Element Particle-in-Cell Simulations of Ion Propulsion. Thesis for the Degree of Doctor of Philosophy, University of Virginia Polytechnic Institute and State, Virginia, 29-55.
[24] Rapp, D. and Francis, W.E. (1962) Charge Exchange between Gaseous Ions and Atoms. Journal of Chemical Physics, 37, 2631-2645. [Google Scholar] [CrossRef] 
[25] Roy, R.I.S., Hastings, D.E. and Gatsonis, N.A. (1996) Ion-Thruster Plume Modeling for Backflow Contamination. Journal of Spacecraft and Rockets, 33, 525-534. [Google Scholar] [CrossRef] 
[26] Sigmund, P. (1969) Theory of Sputtering. I. Sputtering Yield of Amorphous and Polycrystalline Targets. Physical Review, 184, 383-416. [Google Scholar] [CrossRef] 
[27] Katardjiev, I.V., Carter, G. and Nobes, M.J. (1988) Precision Modeling of the Ask-Substrate Evolution during Ion Etching. Journal of Vacuum Science and Technology, A6, 2443-2450. [Google Scholar] [CrossRef] 
[28] Carter, G. (1997) Huygen’s Wavelets and Deterministic Evolution of Surfaces and Interfaces. Vacuum, 48, 925-931. [Google Scholar] [CrossRef] 
[29] Cheng, S.Y.M. (2007) Modeling of Hall Thruster Lifetime and Erosion Mechanisms. Thesis for the Degree of Doctor of Philosophy, Massachusetts Institute of Technology, Cambridge, 39-53.
[30] Yamamura, Y. (1984) An Empirial Formula for Angular Dependence of Sputtering Yields. Radiation Effects, 80, 57-72. [Google Scholar] [CrossRef] 
[31] Yokota, S., Sakoh, D., Matsui, M., et al. (2008) Charge Exchange Ion Number Density Distribution in Hall Thruster Plume. Vacuum, 83, 57-60. [Google Scholar] [CrossRef] 

为你推荐