MHD arcjet onset boundary of high specific impulse Plasma Thrusters-Reference-Cited by-同舟云学术

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MHD arcjet onset boundary of high specific impulse Plasma Thrusters

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Subramanian Jaisankar¹,Sushma T.¹,Sheshadri T.¹

Affiliation:

1. Indian Institute of Science

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-191

Reference9 articles.

1. 1R. G. Jahn, Physics of electric propulsion (McGraw-Hill, New York, 1968) pp.220-221.

2. 84-95.

3. Electrode‐adjacent boundary layer flow in magnetoplasmadynamic thrusters

4. 4J. C. Preble, Onset in Magnetoplasmadynamic Thrusters: A Model of an Electrothermal Instability, M.S. Thesis,De

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