The effect of facility background pressure on hollow cathode operation
Author:
Affiliation:
1. HX5, LLC, NASA Glenn Research Center, Brook Park, Ohio 44124, USA
2. NASA Glenn Research Center, Cleveland, Ohio 44135, USA
Funder
National Aeronautics and Space Administration
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0061045
Reference48 articles.
1. Recent progress in research and development of hollow cathodes for electric propulsion
2. S. J. Hall, T. R. Sarver-Verhey, J. D. Frieman, H. Kamhawi, and J. L. Myers, “Preparation for hollow cathode testing for the advanced electric propulsion system at NASA Glenn Research Center,” paper presented at the 2018 Joint Propulsion Conference, AIAA-2018-4425, Cincinnati, OH, 2018.
3. T. Randolph, V. Kim, H. Kaufman, K. Kozubsky, V. V. Zhurin, and M. Day, “Facility effects on stationary plasma thruster testing,” in 23rd International Electric Propulsion Conference, Seattle, WA, 1993 (IEPC, 1993).
4. Background Pressure Effects on Ion Velocity Distribution Within a Medium-Power Hall Thruster
5. R. R. Hofer and J. R. Anderson, “Finite pressure effects in magnetically shielded Hall thrusters,” in paper presented at the 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cleveland, OH, 2014.
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