Performance comparison of a 9-kW magnetically shielded Hall thruster operating on xenon and krypton
Author:
Affiliation:
1. Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109, USA
Funder
National Science Foundation
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/am-pdf/10.1063/5.0066849
Reference57 articles.
1. Magnetic shielding of a laboratory Hall thruster. I. Theory and validation
2. Magnetic shielding of a laboratory Hall thruster. II. Experiments
3. R. P. Welle, “Xenon and krypton availability for electric propulsion—An updated assessment,” in 29th Joint Propulsion Conference and Exhibit (American Institute of Aeronautics and Astronautics, El Segundo, CA, 1993).
4. T. Kokan and C. R. Joyner, “Mission comparison of Hall effect and gridded ion thrusters utilizing various propellant options,” in AIAA SPACE Conference and Exposition (American Institute of Aeronautics and Astronautics, 2012).
5. D. A. Herman and K. G. Unfried, “Xenon acquisition strategies for high power electric propulsion NASA missions,” in 62nd JANNAF Propulsion Meeting (Joint Army Navy NASA Air Force, Nashville, TN, 2015).
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1. Methods for Mitigating Backsputter in Electric Propulsion Test Facilities II: Beam Halter Demonstration during Hall Thruster Testing;AIAA SCITECH 2024 Forum;2024-01-04
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3. Inferring Electron Heat Flux in a High-Power Hall Thruster with Incoherent Thomson Scattering;AIAA SCITECH 2024 Forum;2024-01-04
4. Erratum: “Performance comparison of a 9-kW magnetically-shielded Hall thruster operating on xenon and krypton” [J. Appl. Phys. 130, 163306 (2021)];Journal of Applied Physics;2023-10-23
5. Evaluation of algebraic models of anomalous transport in a multi-fluid Hall thruster code;Journal of Applied Physics;2023-10-16
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