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Experimental investigations of plasma parameters and species-dependent ion energy distribution in the plasma exhaust plume of a Hall thruster.

机译:霍尔推力器等离子体排气羽中等离子体参数和物种相关离子能量分布的实验研究。

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摘要

For the purpose of understanding and characterizing the behavior of multiply charged propellant ions in a Hall thruster plume, the plasma parameters and ion energy distribution in the SPT-100 plume were studied.; The investigations started with characterizing the plasma properties over an extensive volume of the plume. The distinct peak structures of plasma parameter profiles provided a great insight into the behavior of plume particles. In the very-near-field study, the radial profiles of ion current density, electron temperature, and electron number density were measured. The electron population in the plume was controlled by the competing effects of the two phenomena: the electric and magnetic field influences on the electrons which was dominant very near the thruster exit, and the quasineutrality in the plasma which was dominant farther downstream of the thruster exit. In the near- and far-field study, the angular profiles of ion current density, electron temperature, electron number density, and plasma potential were measured. The original annular structure of the ion beam affected the Plume characteristics in the near-field. Both studies implied the existence of multiply charged propellant ions in the plume.; To characterize the species-dependent ion parameters, an ExB probe was utilized to measure ion energy distributions of each ion species. Each peak in the measured probe traces were curve-fitted with a model based on the kinetic theory of gases to obtain ion energy distribution functions, which provided the exponential factor n of the distribution functions, ion beam energy, ion energy spread, and ion species fraction. The existence of Xe4+ ions in the plume was revealed. The beam energy and ion species fractions data gave rise to a simple ionization and acceleration mechanism in the SPT-100 discharge chamber. The angular profiles of ion species fractions implied that the primary production of Xe1+ ions was clearly separated from the primary production of Xe2+ and Xe 3+ ions by a narrow boundary in the discharge chamber.; These studies provided the most comprehensive collection of plasma parameters in the SPT-100 plume. Also, the ExB technique was the first high-resolution, species-dependent, direct measurements of ion energy distribution in the Hall thruster plume.
机译:为了理解和表征霍尔推进器羽流中多电荷推进剂离子的行为,研究了SPT-100羽流中的等离子体参数和离子能量分布。研究从表征大量羽流的等离子体特性开始。血浆参数曲线的不同峰结构为羽状颗粒的行为提供了很好的见识。在非常近场研究中,测量了离子电流密度,电子温度和电子数密度的径向分布。羽流中的电子种群受两种现象的竞争影响所控制:电场和磁场对电子的影响,该电子在推进器出口附近占主导地位,而等离子体的准中性在推进器出口的下游占主导地位。 。在近场和远场研究中,测量了离子电流密度,电子温度,电子数密度和等离子体电势的角度分布。离子束的原始环形结构影响了近场中的羽流特性。两项研究都暗示羽流中存在带多重电荷的推进剂离子。为了表征与物种有关的离子参数,使用 ExB 探针测量每种离子物种的离子能量分布。使用基于气体动力学理论的模型对所测探针迹线中的每个峰进行曲线拟合,以获得离子能量分布函数,该函数提供了分布函数,离子束能量,离子能量扩散和离子种类的指数因子n分数。揭示了烟羽中Xe 4 + 离子的存在。束能量和离子种类分数数据在SPT-100放电室中产生了简单的电离和加速机制。离子种类组分的角分布表明,Xe 1 + 离子的主要生成与Xe 2 + 和Xe 3+ <离子在放电室中的狭窄边界。这些研究提供了SPT-100羽流中血浆参数的最全面收集。同样, ExB 技术是霍尔推力器羽流中离子能量分布的第一个高分辨率,依赖于物种的直接测量方法。

著录项

  • 作者

    Kim, Sang-Wook.;

  • 作者单位

    University of Michigan.;

  • 授予单位 University of Michigan.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 1999
  • 页码 212 p.
  • 总页数 212
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

  • 入库时间 2022-08-17 11:48:03

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