Investigations of Pole Erosion Mechanisms in the 12.5 kW HERMeS Hall Thruster with the Hall2De Code
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4647
Reference26 articles.
1. Numerical simulations of Hall-effect plasma accelerators on a magnetic-field-aligned mesh
2. The importance of the cathode plume and its interactions with the ion beam in numerical simulations of Hall thrusters
3. Anomalous conductivity in Hall thrusters: Effects of the non-linear coupling of the electron-cyclotron drift instability with secondary electron emission of the walls
4. Study of stationary plasma thrusters using two-dimensional fully kinetic simulations
5. A two-dimensional (azimuthal-axial) particle-in-cell model of a Hall thruster
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1. Impact of low-frequency oscillations on ion energy in a high-power magnetically shielded Hall thruster;Journal of Applied Physics;2022-01-21
2. Research of influence of the additional electrode on Hall thruster plume by particle-in-cell simulation*;Chinese Physics B;2020-09-01
3. Extending service life of hall thrusters: recent progress and future challenges;Reviews of Modern Plasma Physics;2019-11-14
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