Near- and Far-Field Characterization of Stationary Plasma Thruster Plumes
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109-2140
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3703
Reference16 articles.
1. Advanced propulsion system options for geostationary satellites
2. 2Sutton, G. P., Rocket Propulsion Elements, 6th ed.Wiley, New York, 1992, pp.36-38.
3. Technology of closed-drift thrusters
4. Further experimental investigations of a cesium hall-current accelerator
5. Basic studies of a low density Hall current ion accelerator
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