Thermographic investigation of 3.2 mm diameter orificed hollow cathodes
Author:
Affiliation:
1. Michigan, Univ., Ann Arbor
2. NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3793
Reference16 articles.
1. Low-power ion propulsion for small spacecraft
2. A model for mercury orificed hollow cathodes - Theory and experiment
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. Thermal Model of the Hollow Cathode Using Numerically Simulated Plasma Fluxes;Journal of Propulsion and Power;2007-05
2. Status of the Extended Life Test of the Deep Space 1 Flight Spare Ion Engine After 30,000 Hours of Operation;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26
3. Low-Current, Xenon Orificed Hollow Cathode Performance for In-Space Applications;Journal of Propulsion and Power;2003-05
4. Parametric investigation of orifice aspect-ratio on low current hollow cathode power consumption;34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;1998-07-13
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