Long lifetime hollow cathodes for 30-cm mercury ion thrusters
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1976-985
Cited by 17 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. Modeling on plasma energy balance and transfer in a hollow cathode;Journal of Physics D: Applied Physics;2019-05-08
2. Numerical simulation of plasma power deposition on hollow cathode walls using particle-in-cell and Monte Carlo collision method;Physics of Plasmas;2018-10
3. Lifetime Assessment of the NEXT Ion Thruster;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08
4. Thermal Model of the Hollow Cathode Using Numerically Simulated Plasma Fluxes;Journal of Propulsion and Power;2007-05
5. Ion Thruster Development Trends and Status in the United States;Journal of Propulsion and Power;1998-09
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