Plasma Emission Characteristics from a High Current Hollow Cathode-Reference-Cited by-同舟云学术

Plasma Emission Characteristics from a High Current Hollow Cathode

Published:2002-07-07 Issue: Volume: Page:
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Container-title:38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Foster John

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. 1Mantenieks, M.A. and Rawlin, V.K. "Studies of Internal Sputtering in a 30-cm Ion Thruster," 11th Electric Propulsion Conference, New Oreleans, Louisiana, March19-21,1975.

2. 2Rawlin, V.K. "Internal Erosion Rates of a 10-kW Xenon Ion Thruster,"AIAA Paper 88-2913, 24th Joint Propulsion Conference, Boston, Massachusetts, July11-13,1988.

3. 3Brophy, J.R. and Garner, C.E. "Tests of High Current Hollow Cathodes for Ion Engines," AIAA Paper 88-2913, 24th Joint Propulsion Conference, Boston, Massachusetts,July11-13, 1988.

4. High current hollow cathode phenomena

5. 5Latham, P.M., Pearce, A.J., and Bond,R.A. "Erosion Processes in the UK-25 Ion Thruster," IEPC Paper 91-096, 22nd International Electric Propulsion Conference, Viareggio, Italy, October14-17,1991.

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