Design and Initial Tests of a Low Power Radio-Frequency Electrothermal Thruster
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Publisher
American Institute of Aeronautics and Astronautics
Reference11 articles.
1. 1Souliez, F. J., Chianese, S. G., Dizac, G. H., and Micci, M. M. "Low-Power Microwave Arcjet Testing: Plasma and Plum Diagnostics and Performance Evaluation," Micropropulsion for Small Spacecraft, edited by M. M. Micci and A. D. Ketsdever, Vol.147, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2000, pp.199-214.
2. 2Clemens, D.E., Micci, M.M., and Bilén, S.G. "Microwave Electrothermal Thruster Using Simulated Hydrazine," AIAA2006-5156, 42ndAIAA/ASME/SAE/ASEEJointPropulsionConferenceandExhibit,Sacramento,CA,July2006.
3. On the E to H and H to E transition mechanisms in inductively coupled plasma
4. Physics of high-pressure helium and argon radio-frequency plasmas
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