Two-dimensional hybrid model of gradient drift instability and enhanced electron transport in a Hall thruster
Rei Kawashima, Kimiya Komurasaki

TL;DR
This paper develops a 2D hybrid model to analyze gradient drift instability in Hall thrusters, revealing how GDI enhances cross-field electron transport and validating the model against linear theory.
Contribution
A novel 2D hybrid particle-fluid model with a nonoscillatory potential solver for analyzing GDI and electron transport in Hall thrusters.
Findings
Plasma instability with vortex structures observed in simulations.
GDI enhances cross-field electron transport near the channel exit and plume.
Simulation results agree with linear perturbation theory of GDI.
Abstract
An axial-azimuthal two-dimensional Hall thruster discharge model was developed for analyzing gradient drift instability (GDI) and cross-field electron transport enhancement induced solely by the GDI. A hybrid particle-fluid model was used for the partially ionized plasma, where the inertialess electron fluid in the quasineutral plasma was assumed. A nonoscillatory numerical method was proposed for the potential solver in the electron fluid model to avoid numerical instability and analyze the physics of GDI accurately. A simulation is performed for a 1 kW-class anode-layer-type Hall thruster, and the flow field with plasma instability is presented. Plasma instability with vortex-like structures is observed in the acceleration and plume regions. The generated plasma instability enhances the cross-field electron transport in the axial direction around the channel exit and in the plume…
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