A 50 cm diameter annular ion engine
Author:
Affiliation:
1. Electric Propulsion Laboratory, Inc.,Lancaster, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-2716
Reference6 articles.
1. Rawlin, V. K. "Internal Erosion Rates of a 10 kW Xenon Ion ThrusterInn AIAA Paper No. 88-2912, July 1988.
2. "Performance of 10-kW Class Xenon Ion ThrustersrMAIAA Paper No. 88-2914, July 1988.
Cited by 3 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. Integrated hollow cathodes for space applications;34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;1998-07-13
2. Preliminary tests of annular ion optics;28th Joint Propulsion Conference and Exhibit;1992-07-06
3. Thermal mechanical analyses of large diameter ion accelerator systems;25th Joint Propulsion Conference;1989-07-12
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