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Charge exchange ion number density distribution in Hall thruster plume

机译:霍尔推进器羽流中的电荷交换离子数密度分布

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The charge exchange (CEX) ions by the collisions between energetic ions and slow neutral particles in a Hall thruster plume are thought a source of the ions coming back to the satellite. Therefore, mechanical plume shielding has been proposed to prevent the CEX ions from spreading out from near exit region. In order to optimize the shield length, CEX reactions in the plume were evaluated. Number density distributions of neutral particles were measured by the laser absorption spectroscopy (LAS) targeting the absorption line of Xel 823.16 nm (6s[3/2](2)(0) -> 6p[3/2](2)). Ambient neutral gas effect in a test chamber was cancelled out using the measurements at two different back pressures. Measured distribution was compared with the Particle-in-Cell (PIC) and Direct Simulation Monte Carlo (DSMC) analyses. As a result, normalized mean outflow velocity of neutral particles V-z/V-th was identified at 0.6, and the computed CEX ion density was found to be decreased from the channel exit by 50% at 80 mm distance. (c) 2008 Elsevier Ltd. All rights reserved.
机译:霍尔推力器羽流中高能离子与慢速中性粒子之间的碰撞所产生的电荷交换(CEX)离子被认为是回到卫星的离子源。因此,已经提出了机械羽流屏蔽以防止CEX离子从出口区域附近扩散。为了优化屏蔽长度,评估了羽状流中的CEX反应。通过瞄准Xel 823.16 nm(6s [3/2](2)(0)-> 6p [3/2](2))吸收线的激光吸收光谱法(LAS)测量中性粒子的数密度分布。使用在两个不同背压下的测量结果消除了测试室内的环境中性气体效应。将测得的分布与单元中粒子(PIC)和直接模拟蒙特卡洛(DSMC)分析进行了比较。结果,将中性粒子的标准化平均流出速度V-z / V-th确定为0.6,并且发现计算出的CEX离子密度在80mm距离处从通道出口降低了50%。 (c)2008 Elsevier Ltd.保留所有权利。

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