Current Distribution in a Quasisteady MPD Arcjet with Various Anode Geometries
Author:
Affiliation:
1. Institute of Space and Astronautical Science, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.48510
Reference5 articles.
1. Thrust Measurement of KIII MPD Arcjet
2. Transitional Behavior of MPD Arcjet Operation
3. Idealized model for plasma acceleration in an MHD channel
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1. Characterization of a Quasi-Steady Self-Field MPD Thruster with Various Electrode Configurations;AIAA Scitech 2020 Forum;2020-01-05
2. Increasing the effective voltage in applied-field MPD thrusters;Journal of Physics D: Applied Physics;2018-02-01
3. Geometry Effects on the Performance of Cylindrical-Conical (CYLICONE) Plasma Thrusters;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25
4. Numerical simulation of geometric scale effects in cylindrical self-field MPD thrusters;28th Joint Propulsion Conference and Exhibit;1992-07-06
5. Multipole MPD arcjet;International Electric Propulsion Conference;1985-08-17
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