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Anomalous Ion Heating and Pole Erosion in the 12.5-kW Hall Effect Rocket with Magnetic Shielding (HERMeS)

机译:12.5千瓦霍尔效应火箭的异常离子加热和杆侵蚀,磁屏风(HERMES)

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Wear measurements of the inner pole cover in HERMeS have shown as much as ten times higher erosion rates than past numerical simulations predicted. Also, measurements of ion velocity distribution functions (IVDF) suggest that ion heating occurs near the chamfered regions of the acceleration channel and around the inner pole surface. This heating cannot be explained by classical processes (i.e., ionization, charge-exchange and breathing-mode oscillations) alone. In our companion paper we present theoretical evidence that the plasma conditions in this region can excite instabilities in the lower hybrid frequency range. Here, we provide further evidence of their presence through comparisons between numerical simulations and measurements. After including in the 2-D axisymmetric hydrodynamic-PIC code Hall2De an idealized model of the ion temperature based on a scaling with the lower hybrid frequency, we find the agreement between the computed and measured IVDF is significantly improved. In addition, the computed erosion rates at the inner pole surface are now in close agreement with wear test measurements.
机译:Hermes中的内部杆盖的磨损测量显示出比预测的过去数值模拟更高的侵蚀率较高的十倍。而且,离子速度分布函数(IVDF)的测量表明,离子加热在加速度通道的倒角区域附近以及围绕内极面。这种加热不能单独通过经典方法(即电离,电荷交换和呼吸模式振荡)来解释。在我们的伴侣论文中,我们提出了理论上的证据表明该区域的等离子体条件可以在较低的混合频率范围内激发稳定性。在这里,我们通过数值模拟与测量之间的比较提供了进一步的证据。在包括在2-D轴对称水动力学-CIC代码Hall2de基于具有较低混合频率的缩放的离子温度的理想化模型之后,我们发现计算和测量的IVDF之间的协议显着提高。此外,内极面的计算侵蚀速率现在与磨损试验测量密切一致。

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