Applied-Field Magnetoplasmadynamic Thrusters, Part 1: Numerical Simulations Using the MACH2 Code-Reference-Cited by-同舟云学术

Applied-Field Magnetoplasmadynamic Thrusters, Part 1: Numerical Simulations Using the MACH2 Code

Published:2000-09 Issue:5 Volume:16 Page:887-893
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Mikellides Pavlos G.¹,Turchi Peter J.¹,Roderick Norman F.²

Affiliation:

1. Ohio State University, Columbus, Ohio 43235

2. University of New Mexico, Albuquerque, New Mexico 87131

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/10.2514/2.5656

Reference16 articles.

1. Current distribution and plasma acceleration in MPD arcjets with applied magnetic fields

2. Fradkin, D. B. “Analysis of Acceleration Mechanisms and Performance of an Applied Field MPD Arcjet,” Ph.D. Dissertation 1088-T,Dept. of Mechanical and Aerospace Engineering, Princeton Univ., Princeton, NJ,March 1973.

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