Wear trends of the 12.5 kW HERMeS Hall thruster
Author:
Affiliation:
1. NASA Glenn Research Center, Cleveland, Ohio 44135, USA
2. Ohio Aerospace Institute, Cleveland, Ohio 44142, USA
3. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109, USA
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0062579
Reference40 articles.
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4. Plasma simulations in 2-D (r-z) geometry for the assessment of pole erosion in a magnetically shielded Hall thruster
5. B. Jorns, C. A. Dodson, J. R. Anderson, D. M. Goebel, R. R. Hofer, M. J. Sekerak, A. Lopez Ortega, and I. G. Mikellides, “Mechanisms for pole piece erosion in a 6-kW magnetically-shielded Hall thruster,” in 52nd AIAA/SAE/ASEE Joint Propulsion Conference (American Institute of Aeronautics and Astronautics, Reston, VA, 2016), p. 1.
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