Insights from Collisional-Radiative Models of Neutral and Singly Ionized Xenon in Hall Thrusters-Reference-Cited by-同舟云学术

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Insights from Collisional-Radiative Models of Neutral and Singly Ionized Xenon in Hall Thrusters

Published:2022-09 Issue:5 Volume:38 Page:866-879
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Chaplin Vernon H.,Johnson Lee K.,Lobbia Robert B.,Konopliv Mary F.,Simka Timothy,Wirz Richard E.^ORCID

Funder

National Aeronautics and Space Administration

NASA Space Technology Graduate Research Fellowship

Jet Propulsion Laboratory Research Technology Development Innovative Spontaneous Concept program

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B38676

Reference50 articles.

1. FriemanJ. D.KamhawiH.WilliamsG.HermanD.PetersonP. Y.GillandJ.HoferR. “Long Duration Wear Test of the NASA HERMeS Hall Thruster,” AIAA Paper 2018-4645, July 2018. 10.2514/6.2018-4645

2. Lopez OrtegaA.MikellidesI. G.ChaplinV. H.HuangW.FriemanJ. D. “Anomalous Ion Heating and Pole Erosion in the 12.5 kW Hall Effect Rocket with Magnetic Shielding (HERMeS),” AIAA Paper 2020-3620, Aug. 2020. 10.2514/6.2020-3620

3. Growth of the modified two-stream instability in the plume of a magnetically shielded Hall thruster

4. Growth of the lower hybrid drift instability in the plume of a magnetically shielded Hall thruster

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Azimuthal ion dynamics at the inner pole of an axisymmetric Hall thruster;Physics of Plasmas;2024-08-01

2. Analysis of dust charge fluctuations with double-ionized ions and plasma oscillations / instabilities in Hall thrusters;Vacuum;2024-02

3. An optical emission spectroscopy method for determining the electron temperature and density in low-temperature xenon plasma by using a collisional-radiative model considering the hyperfine structure of emission line into metastable state;Spectrochimica Acta Part B: Atomic Spectroscopy;2023-10

4. A xenon collisional-radiative model applicable to electric propulsion devices: III. Determination of the ionization fraction in low-temperature xenon plasma by using ionic and atomic 6p lines;Plasma Sources Science and Technology;2023-09-01

5. 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

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