Performance comparison of a 9-kW magnetically shielded Hall thruster operating on xenon and krypton-Reference-Cited by-同舟云学术

Performance comparison of a 9-kW magnetically shielded Hall thruster operating on xenon and krypton

Published:2021-10-28 Issue:16 Volume:130 Page:163306
ISSN:0021-8979
Container-title:Journal of Applied Physics
language:en
Short-container-title:Journal of Applied Physics

Author:

Su L. L.¹^ORCID,Jorns B. A.¹^ORCID

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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