Author:
Ahedo Eduardo,Raitses Yevgeny
Publisher
American Institute of Aeronautics and Astronautics
Reference17 articles.
1. 1Y. Raitses, D. Staack, L. Dorf, and N.J. Fisch. Experimental study of acceleration region in a 2kW Hall thruster. In39th Joint Propulsion Conference, Huntsville, AL, AIAA 2003-5153. American Institute of Aeronautics and Astronautics,Washington, DC, 2003.
2. Space charge saturated sheath regime and electron temperature saturation in Hall thrusters
3. 4D. Escobar, E. Ahedo, and F. I. Parra. On conditions at the sheath boundaries of a quasineutral code for Hall thrusters. InProc. 29th International Electric Propulsion Conference, Princeton, USA, IEPC-2005-041. Electric Rocket Propulsion Society, Fairview Park, OH, 2005.
4. 5A. Antón and E. Ahedo. New contour algorithms for a Hall thruster hybrid code. In42th Joint Propulsion Conference, Sacramento, CA, AIAA-2006-4834. American Institute of Aeronautics and Astronautics,Washington, DC, 2006.
5. Secondary electron emission from dielectric materials of a Hall thruster with segmented electrodes
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