Preparation for Hollow Cathode Testing for the Advanced Electric Propulsion System at NASA Glenn Research Center
Author:
Affiliation:
1. Vantage Partners, LLC
2. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4425
Reference35 articles.
1. Destructive evaluation of a xenon hollow cathode after a 28,000 hour life test
2. Performance characteristics of the NSTAR ion thruster during an on-going long duration ground test
3. NEXT: NASA's Evolutionary Xenon Thruster
4. Development and Testing of High Current Hollow Cathodes for High Power Hall Thrusters
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2. The effect of facility background pressure on hollow cathode operation;Journal of Applied Physics;2021-09-21
3. Characterization of Propellant Flow and Bias Required to Initiate an Arc Discharge in a Heaterless Hollow Cathode;AIAA Propulsion and Energy 2019 Forum;2019-08-16
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