Two Ways to Evaluate the Xe+ Ion Flow Velocity in a Hall Effect Thruster
Author:
Affiliation:
1. Laboratoire d'Aerothermique
2. University of Paris-Sud
3. ONERA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3949
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Model for the dependence of cathode voltage in a Hall thruster on facility pressure;Plasma Sources Science and Technology;2021-01-01
2. Numerical simulation of the effect of backpressure on the discharge characteristics of a Hall effect thruster;The European Physical Journal D;2020-02
3. Near-Surface Plasma Characterization of the 12.5-kW NASA TDU1 Hall Thruster;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23
4. The Effects of Background Pressure on Hall Thruster Operation;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30
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