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Scaling Laws of Lissajous Acceleration for Electrodeless Helicon Plasma Thruster

机译:无极螺旋等离子推进器的李沙育加速度比例定律

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Analytical thrust model for the Lissajous Helicon Plasma Accelerator (LHPA) is developed by extending previous works [1, 2] in order to guide experiments for achieving feasible value of the thrust. In the LHPA, a rotating transverse electric field in an external divergent magnetic field drives azimuthal currents via electron E × B drift then the thrust is produced due to the Lorentz force. One dimensional (1D) analytical model is developed which includes the electric field penetration into the plasma and the E × B current estimation based on a trajectory analysis. Thrust as a function of parameters of the plasma density and the magnetic field is studied. The penetration of the electrical field into plasmas is examined by 1D particle in cell (PIC) simulations whose results are consistent with those of the 1D analytical model.
机译:通过扩展先前的工作[1、2],建立了李沙育螺线等离子体加速器(LHPA)的分析推力模型,以指导实现可行推力值的实验。在LHPA中,外部发散磁场中的旋转横向电场通过电子E×B漂移驱动方位电流,然后由于洛伦兹力产生推力。开发了一维(1D)分析模型,其中包括电场渗透到等离子体中以及基于轨迹分析的E×B电流估计。研究了推力与等离子体密度和磁场参数的关系。电场渗透到等离子体中的过程是通过1D粒子在细胞(PIC)模拟中进行的,其结果与1D分析模型的结果一致。

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