The University of Michigan
Department of Aerospace Engineering
| Plasmadynamics & Electric Propulsion Laboratory |
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PEPL Thrusters: X2

Above: The X2 nested channel Hall thruster with both channels firing.

Selected Relevant Publications

  1. R. Liang and A. D. Gallimore, "Performance of a Laboratory Hall Thruster with Two Concentric Discharge Channels," 57th JANNAF Propulsion Meeting, 7th Modeling and Simulation, 5th Liquid Propulsion, 4th Spacecraft Propulsion, Joint Subcommittee Meeting, Colorado Springs, CO, May 3-7, 2010.
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