Near-Term High Power Ion Propulsion Options for Earth-Orbital Applications-Reference-Cited by-同舟云学术

Near-Term High Power Ion Propulsion Options for Earth-Orbital Applications

Published:2009-08-02 Issue: Volume: Page:
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Container-title:45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Patterson Michael,Pinero Luis,Sovey James

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. Geosynchronous-Earth-Orbit Communication Satellite Deliveries with Integrated Electric Propulsion

2. 3Patterson, M.J., Benson, S.W., and Soulas, G. C. "NEXT Ion Propulsion System Development Status," JANNAF PublicationSPS-III-14, December 2008.

3. 4Patterson, M.J. "Herakles Thruster Development for the Prometheus JIMO Mission," AIAA Paper No. 2005-3890, 41stJointPropulsion Conference and Exhibit,Tucson AZ, July2005. Flight Hardware

4. 5Williams, G.J. "Results of the 2000 hr Wear Test of the HiPEP Ion Thruster with Pyrolytic Graphite Ion Optics," AIAAPaper No.2006-4668,42nd JointPropulsion Conferenceand Exhibit,Sacramento, CA,July2006.

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