Author:
Kieckhafer Alex,King Lyon
Publisher
American Institute of Aeronautics and Astronautics
Reference19 articles.
1. Tverdokhlebov, O.S., and Semenkin, A.V. "Iodine Propellant for Electric Propulsion - To Be Or Not To Be," 37thAIAA/ASME/SAE/ASEE JointPropulsionConference, Salt Lake City, UT, July, 2001, AIAA2001-3350
2. Bugrova, A.I., Kim, V., et. al. "Physical Processes and Characteristics of Stationary Plasma Thrusters with Closed ElectronsDrift," 22nd InternationalElectricPropulsionConference, Viareggio, Italy, 1991,IEPC-91-079
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