期刊文献+

霍尔推力器通道宽度对电离特性的影响 被引量:2

Influences of discharge channel width on ionization characteristics in Hall thrusters
下载PDF
导出
摘要 为了研究霍尔推力器通道宽度对电离特性的影响,采用以数值模拟为主、实验验证为辅两种手段相结合的方式。所建立的数学模型是基于蒙特卡洛方法的二维完全动力学粒子模型,实验选择了与等离子体无接触的光谱诊断方法。计算和实验两方面的结果都发现随着宽度的增加,电子电离工质气体的速率增加,电离更加有效,而且电离区域变得集中的规律。通过进一步的计算发现,电离特性的明显差异和电子与壁面碰撞频率随宽度增加而减小,电子温度随之升高有着密切关系。电子温度升高一方面会对电离特性起到促进作用,另一方面也会使电离消耗的能量增加。由于稳态时的电子温度是由电子能量平衡机制决定的,因此对电子能量平衡方程进行深入分析之后发现,在研究通道宽度影响电离特性这一物理问题上,电子在壁面上的能量损失是决定电子温度的主导因素,而电离损失仅属于次要因素,宽度增加有利于改善推力器的电离特性。 The ionization characteristics in Hall thrusters with different discharge channel width were investigated by both numerical and experimental methods.Two-dimensional particle-in-cell method based on Monte Carlo collision was utilized for simulation,while no-contact spectrum diagnosis was introduced in the experiment.Both of the calculated and measured results show that with the increasing of channel width,the ionization rate of propulsion increased,the ionization becomes more effective and the ionization area tenas to be more concentrated.Further calculation results indicate that the striking difference of ionization characteristic is closely related to the phenomenon that with the increase of channel width.The collision frequency is reduces between the electron and wall while the electron temperature raises.However,the rising electron temperature not only promotes the neutral ionized but also increases the loss of electron energy.Since the electron temperature in steady state was determined by the electron energy balance mechanism,through analyzing electron energy balance equation,we have found the wall loss is dominant factor affecting the electron temperature when the channel width changes,while the ionization loss was just a subordination factor.The increase of channel width is in favor of improving ionization characteristics.
出处 《推进技术》 EI CAS CSCD 北大核心 2011年第6期806-812,863,共8页 Journal of Propulsion Technology
基金 中国博士后项目(20100471078) 国家杰出青年科学基金(60671012)
关键词 霍尔推力器 通道宽度 电离特性 粒子模拟 光谱诊断 Hall effect thruster Channel width Ionization characteristic Particle-in-cell Spectrum diagnosis
  • 相关文献

参考文献3

二级参考文献62

  • 1黄良甫.电推进系统发展概况与趋势[J].真空与低温,2005,11(1):1-8. 被引量:12
  • 2Zhurin V V, Kaufman H R, Robinson R S. 1999, Plasma Sources Sci. and Technol., 8:R1.
  • 3Yassir Azziz, Manuel Martinez-Sanchez. 2005, Effect of Discharge Voltage on Plume Divergence of a High Specific Impulse Hall Thruster. Presented at the 41st AIAA/ASME/ SAE/ASEE Joint Propulsion Conference &: Exhibit, Tucson, Arizona, USA.
  • 4Raitses Y evgeny, David Staack, Leonid Dorf, et al. 2005, Controlling Ion Acceleration Region in Hall thrusters. Presented at the 29^th International Electric Propulsion Conference, Princeton University, New Jersey, USA.
  • 5Bechu S, Gascon N, Roche S, et al. 2000, Comparison between Two Kinds of SPTs: SPT100 and ATON. Presented at the 36^th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Huntsville, Alabama, USA.
  • 6Michael Keidar, lain D Boyd. 1999, Journal of Applied Physics, 86:4786.
  • 7Corey Ronald L, Snyder John Steven, Price Xenophon, et al. 2008, Journal of Spacecraft and Rockets, 45:766.
  • 8Iain D Boyd, John T Yim. 2004, Journal of Applied Physics, 95:4575.
  • 9Fruchtman A. and Cohen-Zur A. 2004, Plume Divergence in the Hall Thruster. Presented at the 40^th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit., Fort Lauderdale, Florida, USA.
  • 10Yu Daren, Wu Zhiwen, E Peng, et al. 2005, Engineering Science, 7:22.

共引文献108

同被引文献11

引证文献2

二级引证文献2

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