Collisional-Radiative Models of Neutral and Singly-Ionized Xenon in Hall Thrusters: Experimental Validation and Model Investigations
Author:
Affiliation:
1. University of California, Los Angeles
2. Jet Propulsion Laboratory, California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-3390
Reference11 articles.
1. Passive optical diagnostic of Xe propelled Hall thrusters. II. Collisional-radiative model
2. A xenon collisional-radiative model applicable to electric propulsion devices: II. Kinetics of the 6s, 6p, and 5d states of atoms and ions in Hall thrusters
3. A xenon collisional-radiative model applicable to electric propulsion devices: I. Calculations of electron-impact cross sections for xenon ions by the Dirac B-spline R-matrix method
4. Near-infrared collisional radiative model for Xe plasma electrostatic thrusters: the role of metastable atoms
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1. Fast Optical Emission Spectroscopy Measurements of Time-Resolved Electron Temperature in a Hall Thruster;AIAA SCITECH 2024 Forum;2024-01-04
2. Accuracy of using metastable state measurements in laser-induced fluorescence diagnostics of xenon ion velocity in Hall thrusters;Plasma Sources Science and Technology;2023-01-01
3. Insights from Collisional-Radiative Models of Neutral and Singly Ionized Xenon in Hall Thrusters;Journal of Propulsion and Power;2022-09
4. Insights from Collisional-Radiative Models of Neutral and Singly-Ionized Xenon in Hall Thrusters;AIAA Propulsion and Energy 2021 Forum;2021-07-28
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