Impact of Excitation and Reaction Processes on the Field Reversed Configuration Thruster Efficiency
Author:
Affiliation:
1. University of Colorado, Colorado Springs
2. ERC, Inc.
3. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2630
Reference27 articles.
1. Particle Confinement Scaling in Field-Reversed Configurations
2. Classical transport in a field reversed configuration
3. 3Elliott F., Foster J., and Patterson M., An Overview of the High Power Electric Propulsion (HiPEP) Project, AIAA Paper 2004-3453.
4. 4Kirtley D., Brown D., and Gallimore A. Details on an annular field reversed configuration plasma device for spacecraft propulsion, IEPC-2005-171.
5. 5Miller S., Rovey J. Progress in modeling of pre-ionization and geometric effects on a field-reversed configuration plasma thruster, AIAA 2009-3733.
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