NASA's Evolutionary Xenon Thruster (NEXT) Long-Duration Test as of 736 kg of Propellant Throughput-Reference-Cited by-同舟云学术

NASA's Evolutionary Xenon Thruster (NEXT) Long-Duration Test as of 736 kg of Propellant Throughput

Published:2012-07-30 Issue: Volume: Page:
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Container-title:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Shastry Rohit,Herman Daniel,Soulas George,Patterson Michael

Publisher

American Institute of Aeronautics and Astronautics

Reference49 articles.

1. 1Patterson, M. J. and Benson, S. W. "NEXT Ion Propulsion System Development Status and Performance," AIAA-2007-5199, 43rdAIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cincinnati, OH, July8-11,2007.

2. 4Brophy, J. R. "Development and Testing of the Dawn Ion Propulsion System," AIAA-2006-4319, 42ndAIAA/ASME/SAE/ASEE JointPropulsion Conference and Exhibit, Sacramento, CA, July9-12,2006.

3. 5Benson,S.W.andPatterson,M.J."NASA'sEvolutionaryXenonThruster(NEXT)IonPropulsionTechnology Development Status in 2009," IEPC-2009-150, 31stInternational Electric Propulsion Conference, Ann Arbor, MI, September20-24,2009.

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