Hall current plasma accelerator
Author:
Affiliation:
1. Electro-Optical Systems, Inc., Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2527
Reference11 articles.
1. Tecnical Notes
Cited by 28 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. Review of alternative propellants in Hall thrusters;Acta Astronautica;2023-11
2. Long-Duration Test of Coaxial Low-Energy Surface Flashover Ignitor;Journal of Propulsion and Power;2023-09
3. Low energy surface flashover for initiation of electric propulsion devices;Plasma Research Express;2019-01-11
4. Low frequency azimuthal stability of the ionization region of the Hall thruster discharge. I. Local analysis;Physics of Plasmas;2014-04
5. History of Electric Propulsion at NASA Glenn Research Center: 1956 to Present;Journal of Aerospace Engineering;2013-04
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