Low-Current, Xenon Orificed Hollow Cathode Performance for In-Space Applications
Author:
Affiliation:
1. NASA Glenn Research Center, Cleveland, Ohio 44135
2. University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.6127
Reference21 articles.
1. Low-power ion propulsion for small spacecraft
2. Siegfried, D. E. “A Phenomenological Model for Orificed Hollow Cathodes,” Ph.D. Dissertation,Dept. of Mechanical Engineering, Colorado StateUniv., Fort Collins, CO,1983.
3. Salhi, A. “Theoretical and Experimental Studies of Orificed, Hollow Cathode Operation,” Ph.D. Dissertation,Dept. of Aeronautical and Astronautical Engineering, Ohio StateUniv., Columbus, OH,1993.
4. A Mercury plasma-bridge neutralizer.
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