Performance of a modified downstream-cathode MPD thruster.
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27738
Reference3 articles.
1. Exploratory tests on a downstream-cathode MPD thruster
2. Feasibility Studies on an Auxiliary Propulsion System Using MPD Thrusters
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1. Applied-Field Magnetoplasmadynamic Thrusters for Orbit-Raising Missions;Orbit-Raising and Maneuvering Propulsion: Research Status and Needs;1984-01-01
2. Experimental Studies on a Low-Power Duoplasmatron-Type MPD Thruster;Journal of Spacecraft and Rockets;1977-08
3. Experimental studies on a low-power MPD thruster of duoplasmatron type;12th International Electric Propulsion Conference;1976-08-16
4. Survey of Electric Propulsion Capability;Journal of Spacecraft and Rockets;1975-11
5. Survey of electric propulsion capability;10th Propulsion Conference;1974-08-16
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