Design and fabrication of a flight model 2.3 kW ion thruster for the Deep Space 1 Mission
Author:
Affiliation:
1. Hughes Corp., Electron Dynamics Div., Torrance, CA
2. NASA, Lewis Research Center, Cleveland, OH
3. JPL, Pasadena, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3327
Reference19 articles.
1. 2Sovey, J.S., etal, "Development of an Ion Thruster and Power Processor for New Millennium's Deep Space 1Mission,"AIAA Paper 97-2778, July 1997.
2. NASA 30 cm ion thruster development status
3. 5Patterson, M.J., etal,"2.3 kW Ion Thruster Wear Test,"AIAApaper 95-2516,July 1995.
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