Impact of low-frequency oscillations on ion energy in a high-power magnetically shielded Hall thruster
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109, USA
Funder
National Aeronautics and Space Administration
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0067325
Reference38 articles.
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2. K. De Grys, A. Mathers, B. Welander, and V. Khayms, “Demonstration of 10,400 hours of operation on a 4.5 kW qualification model Hall thruster,” in 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Nashville, TN (AIAA, 2010), AIAA 2010-6698.
3. Magnetic shielding of a laboratory Hall thruster. I. Theory and validation
4. Magnetic shielding of a laboratory Hall thruster. II. Experiments
5. A. Lopez Ortega and I. G. Mikellides, “Investigations of pole erosion mechanisms in the 12.5 kW HERMeS Hall thruster using numerical simulations and ion velocity measurements,” in AIAA Propulsion and Energy Forum, 2018 Joint Propulsion Conference, Cincinnati, OH (AIAA, 2018), AIAA 2018-4647.
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