MPD thruster performance - Propellant distribution and species effects-Reference-Cited by-同舟云学术

MPD thruster performance - Propellant distribution and species effects

Published:1986-07 Issue:4 Volume:2 Page:317-322
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Merfeld D. J.¹,Kelly A. J.¹,Jahn R. G.¹

Affiliation:

1. Princeton University, Princeton, New Jersey

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/10.2514/3.22889

Reference7 articles.

1. 2Rudolph, L. K. "The MPD Thruster Onset Current Performance Limitation," Ph.D. Thesis, Mechanical and Applied Engineering Dept.Princeton University, Princeton, NJ,Sept. 1980.

2. 3Boyle, M. J. "Acceleration Processes in the Quasi-Steady Magnetoplasmadynamic Discharge," Ph.D. Thesis, Mechanical and Applied Engineering Dept.Princeton University, Princeton, NJ,Oct. 1974.

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

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