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Particle-in-cell simulations of Hall thruster acceleration and near plume regions

机译:霍尔推进器加速度和羽流区域附近的粒子 - 细胞模拟

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The results of 1-D azimuthal, and 2-D z-theta, particle-in-cell simulations of Hall thruster acceleration and near plume regions are reported. The 1-D simulations show that fast moving electron waves drive coherent, large amplitude, ion acoustic waves. The ion waves become azimuthally coherent too quickly for ion sound to be the cause; the coherence comes from early electron waves. 2-D simulations with only fast moving, main beam, ions result in ion acoustic wave amplitudes much lower than those in the 1-D calculations. The addition of a small amount of ionization in the domain, at a rate consistent with Hall thruster parameters, causes the potential profile to divide into two distinct regions. In the upstream portion of the domain, the potential profile is very steep; in the downstream portion, the potential profile is almost flat. Electron transport in the two regions is discussed. Published by AIP Publishing.
机译:据报道了1-D方位角和2-D Z-THETA,霍尔推进器加速度和附近羽流区域的细胞内仿真的结果。 1-D模拟显示快速移动的电子波驱动相干,大振幅离子声波。 离子波对离子声音变得非常迅速,因为离子声音是原因; 相干性来自早期电子波。 2-D模拟只有快速移动,主梁,离子导致离子声波幅度远低于1-D计算中的离子声波幅度。 在与霍尔推进器参数一致的速率下,在域中添加少量电离导致潜在的曲线分为两个不同的区域。 在域的上游部分中,潜在的概况非常陡峭; 在下游部分,潜在的轮廓几乎是平坦的。 讨论了两个地区的电子传输。 通过AIP发布发布。

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