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Diagnosing on plasma plume from xenon Hall thruster with collisional-radiative model

机译:基于碰撞辐射模型的氙气霍尔推进器等离子体羽诊断

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The collisional-radiative model for xenon is used to calculate the electron density and temperature, and the atom population distribution in the plasma plume from a xenon Hall thruster. In the calculation, 173 levels of atom population are considered; only the processes of electron induced excitation and deexcitation, and spontaneous decay are simulated. The plasma plume is assumed to be optically thin. Consequently, the reasonable parameters of plasma plume along the outside center line of the thruster channel are obtained by making the calculated emission spectrum corresponding to measured ones and based on the atomic data available on site and by codes.
机译:氙的碰撞辐射模型用于计算电子密度和温度,以及氙霍尔推力器产生的等离子羽流中的原子种群分布。在计算中,考虑了173个原子级。仅模拟了电子感应的激发和反激发以及自发衰减的过程。假定等离子羽流光学上很薄。因此,通过使计算出的发射光谱与测量的发射光谱相对应,并基于现场可用的原子数据和代码,可以获得沿推进器通道外部中心线的等离子羽流的合理参数。

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