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Experimental Studies of the High-Frequency Oscillation Structure in the Discharge Channel of a Hall Thruster in Two Stable Discharge Modes

机译:两种稳定排放模式下霍尔推进器放电通道高频振荡结构的实验研究

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摘要

The structure of high-frequency oscillations in the plasma of a Hall thruster (HT) is studied experimentally in two different stable discharge modes: the "jet" mode and the "bell" mode. The discharge modes under study differ in the geometrical shape of the plasma plume and in the main integral characteristics of the thruster, such as the anode efficiency, driving force, and the specific momentum and thermal conditions of the construction achieved at almost identical input parameters. The studies are mainly performed in the frequency range of 5 to 150 MHz. It is shown that, in this frequency range, the oscillations represent the set of the azimuthal wave harmonics that propagate in the direction coinciding with the electron drift direction and obey the almost linear dispersion relation. An explicit correlation is found between the spectral composition of the waves and the type of the discharge mode.
机译:实验研究了霍尔推进器(HT)等离子体中的高频振荡结构,以两种不同的稳定排放模式研究:“喷射”模式和“钟形”模式。 研究的放电模式在等离子体羽流的几何形状和推进器的主要整体特征中不同,例如阳极效率,驱动力以及在几乎相同的输入参数上实现的结构的特定动量和热条件。 研究主要在5至150 MHz的频率范围内进行。 结果表明,在该频率范围内,振荡表示在与电子漂移方向一致的方向上传播的方位波谐波的一组,并遵循几乎线性色散关系。 在波的光谱组合物和放电模式的类型之间找到显式相关性。

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