Simulations of Lithium Lorentz Force Accelerator (LiLFA) Plasma Flows-Reference-Cited by-同舟云学术

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Simulations of Lithium Lorentz Force Accelerator (LiLFA) Plasma Flows

Published:2003-06-26 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Sankaran Kamesh¹,Choueiri Edgar¹,Jardin Stephen¹

Affiliation:

1. Princeton University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4843

Reference35 articles.

1. L. K. Rudolph. The MPD Thruster Onset Current Performance Limitation. PhD thesis,Princeton U.,1980.

2. D.D.Ho. ErosionStudiesina(MPD)Thruster. Master's thesis, Princeton U.,1981.

3. D. I. Kaplan. Performance Chatacteristics of Geometrically-Scaled Magnetoplasmadynamic (MPD) Thrusters. Master's thesis, Princeton U.,1982.

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