The University of Michigan
Department of Aerospace Engineering
| Plasmadynamics & Electric Propulsion Laboratory |
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PEPL Thrusters: NASA-173Mv2

Above: Photograph of the NASA-173Mv2 operating at 300 V, 10 mg/s (from ref. 1).

Above: Photograph of the NASA-173Mv2 prior to testing (from ref. 1).

Selected Relevant Publications

  1. Hofer, R. R., "Development and Characterization of High-Efficiency, High-Specific Impulse Xenon Hall Thrusters," Ph.D. Dissertation, University of Michigan, 2004.
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