Design of Miniature Ring-Cusp Ion Thrusters via Analysis of Discharge EEDF and Plasma Parameter Mapping
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4545
Reference19 articles.
1. Design Study for a Planet-Finding Space Interferometer
2. Hollow Cathode and Low-Thrust Extraction Grid Analysis for a Miniature Ion Thruster
3. Ion source discharge performance and stability
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1. Revealing the plasma confinement behavior of an axial ring cusp hybrid discharge in a miniature ion thruster using PIC/MCC simulation;Plasma Sources Science and Technology;2023-08-01
2. A neural network model relating extraction current characteristics with optical emission spectra for the purpose of a digital twin of miniaturized ion thrusters;Journal of Physics D: Applied Physics;2022-04-07
3. Numerical investigation of plasma behavior in a micro DC ion thruster using the particle-in-cell/Monte Carlo collision (PIC/MCC) method;Journal of Physics D: Applied Physics;2021-08-20
4. Computational Modeling of an Axial Ring Cusp Hybrid Discharge for the MiXI Thruster;2018 Joint Propulsion Conference;2018-07-08
5. DC-Ion Model Validation and Convergence Studies;2018 Joint Propulsion Conference;2018-07-08
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