Electron Number Density and Temperature in MPD-Arc Thruster Exhausts
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50381
Reference2 articles.
1. Exhaust flow and propulsion characteristics of a pulsed MPD arc thruster
2. Exhaust Characteristics of a Megawatt Nitrogen MPD-ARC Thruster
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