Propellant Thermal Management Effect on Neutral Residence Time in Low-Voltage Hall Thrusters
Author:
Affiliation:
1. Department of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332
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.B34702
Reference38 articles.
1. Geosynchronous-Earth-Orbit Communication Satellite Deliveries with Integrated Electric Propulsion
2. Efficiency Analysis of a Hall Thruster Operating with Krypton and Xenon
3. The effect of discharge chamber wall temperature on ion thruster performance
4. Performance and Active Thermal Control of a 2-kW Hall Thruster with Segmented Electrodes
5. Effect of Anode Temperature on Hall Thruster Performance
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