Review of the NASA's Evolutionary Xenon Thruster (NEXT) Long-Duration Test as of 632 kg of Propellant Throughput-Reference-Cited by-同舟云学术

Review of the NASA's Evolutionary Xenon Thruster (NEXT) Long-Duration Test as of 632 kg of Propellant Throughput

Published:2011-07-31 Issue: Volume: Page:
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Container-title:47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Herman Daniel

Publisher

American Institute of Aeronautics and Astronautics

Reference50 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, July 8-11,2007.

2. 4Brophy, J. R. "Development and Testing of the Dawn Ion Propulsion System," AIAA-2006-4319, 42ndAIAA/ASME/SAE/ASEEJoint Propulsion Conferenceand Exhibit, Sacramento,CA, July 9-12,2006.

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, September 20-24,2009.

4. 6Soulas, G. C. "NEXT Single String Integration Test Results," AIAA-2009-4816, 45thAIAA/ASME/SAE/ASEEJoint Propulsion Conferenceand Exhibit,Denver,CO,August2-5,2009.

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