Exhaust Flow and Propulsion Characteristics of a Pulsed MPD-Arc Thruster
Author:
Affiliation:
1. NASA Lewis Research Center, Clevelahd, Ohio
2. Pennsylvania State University, University Park, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50494
Reference4 articles.
1. Pressure Measurements in the Exhaust of a Pulsed Megawatt MPD Arc Thruster
2. Electron Number Density and Temperature in MPD-Arc Thruster Exhausts
3. Investigations on plasma thrusters with thermal and self-magnetic acceleration.
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