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Alec D. Gallimore

Professor
Aerospace Engineering
University of Michigan
United States of America

Biography

Alec D. Gallimore, Robert J. Vlasic Dean of Engineering, Richard F. and Eleanor A. Towner Professor of Engineering, formerly Associate Dean for Research and Graduate Education from 2011 to 2013 and Associate Dean for Academic Affairs in the College of Engineering from 2013-2016. He is a member of the Applied Physics graduate program; from 2005 to 2011, Professor Gallimore served as an Associate Dean at the Horace H. Rackham School of Graduate Studies where he was the Graduate School liaison to Michigan’s graduate programs in engineering, the physical sciences, and mathematics. Professor Gallimore’s primary research interests include electric propulsion, plasma diagnostics, space plasma simulation, electrode physics, nano-particle energetics and hypersonic aerodynamics/plasma interaction. He has extensive design and testing experience with a number of electric propulsion devices including Hall thrusters, ion thrusters, RF thrusters, microwave thrusters, arcjets, 100-kW-class steady MPD thrusters and multimegawatt pulsed coaxial plasma accelerators. He has implemented a variety of probe, microwave, and optical/laser plasma diagnostics, and has graduated 36 PhD students and 14 MS students in the fields of electric propulsion and plasma physics. Professor Gallimore has written more than 300 archival journal articles and conference papers, and 2 book chapters. He is also director of the NASA-funded Michigan Space Grant Consortium and director of the Michigan/Air Force Center of Excellence in Electric Propulsion. Professor Gallimore has served on a number of NASA and Department of Defense boards and studies, including being a member of the United States Air Force Scientific Advisory Board.

Research Interest

Electric Propulsion Space Propulsion Plasma Physics

Publications

  • Gulczinski, F. S. and Gallimore, A. D., “Near Field Ion Energy and Species Measurements of a 5 kW Laboratory Hall Thruster ” Journal of Propulsion and Power (AIAA), Vol. 17, No. 2, March-April 2001, 418-427.

  • Haas, J. M., and Gallimore, A. D., “Internal Plasma Potential Profiles in a Laboratory-Model Hall Thruster,” Physics of Plasmas, Vol. 8, No. 2, February 2001, 652-660.

  • King, L. B., and Gallimore, A. D., “Mass Spectral Measurements in the Plume of an SPT-100 Hall Thruster,” Journal of Propulsion and Power (AIAA), Vol. 16, No. 6, November-December 2000, 1086-1092.

  • Haas, J. M., Gallimore, A. D., and McFall, K., and Spanjers, G., “Development of a High-Speed, Reciprocating Electrostatic Probe System for Hall Thruster Interrogation,” Review of Scientific Instruments, Vol. 71, No. 11, November 2000, 4131-4138.

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