Design and performance of an annular magnetoplasmadynamic thruster-Reference-Cited by-同舟云学术

Design and performance of an annular magnetoplasmadynamic thruster

Published:1991-11 Issue:6 Volume:7 Page:975-980
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Heimerdinger D. J.¹,Martinez-Sanchez M.²

Affiliation:

1. Institute for Defense Analyses, Alexandria, Virginia 22311

2. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139

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/10.2514/3.23416

Reference17 articles.

1. 2Cobine, J. D., Gaseous Conductors, Dover Publications, New York, 1958.

2. 3Rudolph, L. K., and Jahn, R. G. "The MPD Thruster Onset Current Performance Limitation," Ph.D. Dissertation,Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ,1980.

3. Effect of Self-Magnetic Forces on the Anode Mechanism of a High Current Discharge

4. Thrust Measurement of KIII MPD Arcjet

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