100 kWe MPD thruster system design
Author:
Affiliation:
1. California Institute of Technology, Jet Propulsion Laboratory, Pasadena, CA
2. Martin Marietta Aerospace, Denver, CO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-1897
Reference44 articles.
1. R.P. Nagorski and R.J. Boain, "An Evaluation o f Nuclear E l e c t r i c Propulsion f o r Planetary Exploration," AIAA Paper No. 81-0705.
2. F.A. Jackson, J.C. Stansel, D. Jortner. and C.F. Hageberg. "An Operational Electrothermal Propulsion System For Spacecraft Reaction Control," AIAA Paper No. 66-21?
3. W.R. Kerslake and L.R. Ignaczak, "SERT I 1 1980 Extended Thruster Experiments ,la AIAA 81-06605. 1981.
4. Origin of the electron-bombardment ion thruster
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1. A Comparison of Electric Propulsion Technologies for Orbit Transfer;Orbit-Raising and Maneuvering Propulsion: Research Status and Needs;1984-01-01
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