The University of Michigan
Department of Aerospace Engineering
| Plasmadynamics & Electric Propulsion Laboratory |
Loading
PEPL Thrusters: X3

Above: The X3 nested-channel Hall thruster with all three channels firing at 30 kW total discharge power.

Selected Relevant Publications

  1. Hall, S.J., Cusson, S.E., Gallimore, A.D., "30-kW Performance of a 100-kW Class Nested-Channel Hall Thruster", IEPC 2015-125 , 34th International Electric Propulsion Conference, Kobe, Japan, July 6-10, 2015.
  2. Hall, S., Gallimore, A., Kamhawi, H., Brown, D., Polk, J., Goebel, D., Hofer, R., "Implementation and Initial Validation of a 100-kW Class Nested-channel Hall Thruster", AIAA 2014-3815 , 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, OH, July 28-30, 2014.
  3. Florenz, R., Hall, S., Gallimore, A., Kamhawi, H., Griffiths, C., Brown, D., Hofer, R., Polk, J., "First Firing of a 100-kW Nested-channel Hall Thruster," IEPC-2013-394, 33rd International Electric Propulsion Conference, Washington, D.C., October 6-10, 2013.
All rights reserved, copyright ©
Page Last Modified: Saturday, 23-Jan-2016 01:00:57 EST
PEPL is part of the University of Michigan, Department of Aerospace Engineering.
Feedback and questions about PEPL and this web site may be directed to the laboratory director, webmaster, or the laboratory land line, (734)764-4199.