Bismuth propellant option for very high power TAL thruster
Author:
Affiliation:
1. TsNIIMASh, Korolev, Russia
2. JPL, Pasadena, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-348
Reference8 articles.
1. High power Hall thrusters
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