Comparison of Simulated Magnetoplasmadynamic Thruster Flowfields to Experimental Measurements-Reference-Cited by-同舟云学术

Comparison of Simulated Magnetoplasmadynamic Thruster Flowfields to Experimental Measurements

Published:2005-01 Issue:1 Volume:21 Page:129-138
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Sankaran K.¹,Choueiri E. Y.¹,Jardin S. C.¹

Affiliation:

1. Princeton University, Princeton, New Jersey 08544

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/10.2514/1.5340

Reference42 articles.

1. 1Rudolph, L. K. "The MPD Thruster Onset Current Performance Limitation," Ph.D. Dissertation, Mechanical and Aerospace Engineering Dept.Princeton Univ., Princeton, NJ,1980.

2. 2Ho, D. D. "Erosion Studies in a (MPD) Thruster," M.S. Thesis, Mechanical and Aerospace Engineering Dept.Princeton Univ., Princeton, NJ,1981.

3. 3Kaplan, D. I. "Performance Chatacteristics of Geometrically-Scaled Magnetoplasmadynamic (MPD) Thrusters," M.S. Thesis, Mechanical and Aerospace Engineering Dept.Princeton Univ., Princeton, NJ,1982.

4. 4Wolff, M. J. "A High Performance Magnetoplasmadynamic Thruster," M.S. Thesis, Mechanical and Aerospace Engineering Dept.Princeton Univ., Princeton, NJ,1984.

5. 5Gilland, J. H. "The Effect of Geometric Scale upon MPD Thruster Behavior," M.S. Thesis, Mechanical and Aerospace Engineering Dept.Princeton Univ., Princeton, NJ,1988.

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