Numerical modeling of the flow discharge in MPD thrusters-Reference-Cited by-同舟云学术

Numerical modeling of the flow discharge in MPD thrusters

Published:1989-01 Issue:1 Volume:5 Page:49-55
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Auweter-Kurtz M.¹,Kurtz H. L.¹,Schrade H. O.¹,Sleziona P. C.¹

Affiliation:

1. Universitat Stuttgart, Stuttgart, Federal Republic of Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.23114

Reference13 articles.

1. 2King, D. Q. "Magnetoplasmsadynamic Channel Flow for Design of Coaxial MPD Thrusters," Ph.D. Dissertation,Dept. of Mechanical and Aerospace Engineereing, Princeton Univ. July 1981.

2. Current distribution on the electrodes of MPD arcjets

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