Design and fabrication of a flight model 2.3 kW ion thruster for the Deep Space 1 Mission-Reference-Cited by-同舟云学术

Design and fabrication of a flight model 2.3 kW ion thruster for the Deep Space 1 Mission

Published:1998-07-13 Issue: Volume: Page:
ISSN:
Container-title:34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Christensen Jon¹,Freick Kenneth¹,Hamel David¹,Hart Stephen¹,Norenberg Kirk¹,Haag Thomas²,Patterson Michael²,Rawlin Vincent²,Sovey James²,Anderson John³,e al

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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