Thermal Model of the Hollow Cathode Using Numerically Simulated Plasma Fluxes
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.21103
Reference21 articles.
1. Status of the Extended Life Test of the Deep Space 1 Flight Spare Ion Engine After 30,000 Hours of Operation
2. Destructive evaluation of a xenon hollow cathode after a 28,000 hour life test
3. Extending Hollow Cathode Life for Electric Propulsion for Long-Term Missions
4. Long lifetime hollow cathodes for 30-cm mercury ion thrusters
5. Thermographic investigation of 3.2 mm diameter orificed hollow cathodes
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2. A Coupled 0-D Plasma Thermal Model for Hollow Cathodes;IEEE Transactions on Plasma Science;2023-03
3. Plasma hollow cathodes;Journal of Applied Physics;2021-08-07
4. Critical implications of ion-surface energy accommodation and neutralization mechanism in hollow cathode physics;Journal of Applied Physics;2021-07-28
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