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Simulations of Electron Heating in a Capacitively Coupled Radio Frequency Micro-Thruster using Computational Fluid Dynamics

机译:使用计算流体动力学的电容耦合射频微推进器中的电子加热模拟

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A 2D fluid simulation of a capacitively coupled radio frequency (rf) electrothermal plasma micro-thruster has been performed using the CFD-ACE package for a preliminary analysis of the localized electron heating profiles. A 1.5 Torr argon plasma with 10 W (V_o=240 V) power input at 13.56 MHz was modeled assuming a Maxwellian electron distribution with a secondary electron emission co-efficient of 0.1. During the rf cycle, hot ion-induced secondary electrons with energies of 33 eV were responsible for most ionization and excitation events. The peak plasma density reached 4×10~(18) m~(-3), matching previous global model density estimates to within a factor of two. A 1D fluid simulation matching a previously benchmarked PIC code simulation was also performed as a validation tool for the 2D simulation.
机译:已经使用CFD-ACE封装进行了电容耦合射频(RF)电热等离子体微推进器的2D流体模拟,以进行局部电子加热型材的初步分析。假设最大电子发射的最大电子发射的最大电子发射有0.1的最高电子发射的1.5托的氩气相对于13.56MHz的电力输入为13.56MHz。在RF循环期间,具有33eV的能量的热离子引起的二次电子负责大多数电离和激发事件。峰值等离子体密度达到4×10〜(18)m〜(-3),匹配以前的全局模型密度估计到两个倍数。匹配先前基准的PIC代码仿真的1D流体仿真也被作为2D仿真的验证工具进行。

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