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Azimuthal instability of MPD thruster plasmas and inception of critical regimes

机译:MPD推进器等离子体的方位角不稳定性和临界状态的开始

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Magnetoplasmadynamic thrusters are known to enter a strongly unstable operating regime when operated at high ratios of total squared current over propellant mass flow rate. This regime, simply named onset, sets a limit to the propulsive effectiveness of these thrusters, as it leads to thrust efficiency degradation and intense damage of thruster components. Despite various theories have been put forward to explain this phenomenon, we still lack a complete and definitive understanding. In this work we investigate the possibility that this critical regime can be explained in terms of a series of events starting with the breaking of the azimuthal symmetry of the flow and then leading to the experimentally observed oscillations of thruster voltage by means of either variations of thruster inductance or fluctuations of the voltage across the anode sheath. We show that in both cases the so called filamentation of the plasma, i.e. the redistribution of the homogeneous plasma into tiny plasma channels, can be accounted as one of the main triggers of the onset regime.
机译:已知当以总平方电流与推进剂质量流率的高比率进行操作时,磁等离子体动力推进器会进入非常不稳定的运行状态。这种机制(简称为“发作”)为这些推进器的推进效能设置了限制,因为它会导致推进效率降低和推进器组件的严重损坏。尽管提出了各种理论来解释这种现象,但我们仍然缺乏完整和确定的理解。在这项工作中,我们研究了可以用一系列事件来解释这种临界状态的可能性,这些事件始于流动的方位角对称性的破坏,然后通过推进器的任一种变化导致实验上观察到的推进器电压的振荡电感或阳极护套两端的电压波动。我们表明,在两种情况下,所谓的血浆丝化,即均质血浆重新分布到微小的血浆通道中,都可以被认为是发病机制的主要诱因之一。

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