Influence of the magnetic field's curvature on the radial-azimuthal dynamics of a Hall thruster plasma discharge with different propellants
Maryam Reza, Farbod Faraji, and Aaron Knoll

TL;DR
This study investigates how the curvature of magnetic fields affects plasma behavior in Hall thrusters, revealing significant impacts on plasma instabilities, temperature distributions, and ion beam divergence across different propellants.
Contribution
The paper provides a detailed 2D analysis of magnetic field curvature effects on plasma dynamics in Hall thrusters, including comparisons with 1D simulations and across multiple propellants.
Findings
Positive curvature favors Electron Cyclotron Drift Instability.
Negative curvature enhances Modified Two Stream Instability.
Magnetic curvature significantly affects ion beam divergence.
Abstract
The topology of the applied magnetic field is an important design aspect of Hall thrusters. For modern Hall thrusters, the field topology most often features curved lines with a concave (negative) curvature upstream of the field peak and a convex (positive) curvature downstream. Additionally, the advent of the magnetic shielding technique has resulted in the design of Hall thrusters with non-conventional magnetic fields that exhibit high degrees of concavity upstream of the field's peak. We carry out a rigorous and detailed study of the effects that the magnetic field's curvature has on the plasma properties and the underlying processes in a 2D configuration representative of a Hall thruster's radial-azimuthal cross-section. The analyses are performed for plasma discharges of three propellants: xenon, krypton, and argon. For each propellant, we have carried out high-fidelity…
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Taxonomy
TopicsPlasma Diagnostics and Applications · Dust and Plasma Wave Phenomena · Electrohydrodynamics and Fluid Dynamics
