Theoretical treatment of current, mass flow, and related distributions in MPD plumes-Reference-Cited by-同舟云学术

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Theoretical treatment of current, mass flow, and related distributions in MPD plumes

Published:1972-04-17 Issue: Volume: Page:
ISSN:
Container-title:9th Electric Propulsion Conference
language:
Short-container-title:

Author:

KRUELLE G.¹

Affiliation:

1. Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt, Institut fuer Plasmadynamik, Stuttgart, West Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1972-501

Reference6 articles.

1. Experimental results in high-specific-impulse thermoionic acceleration

2. Brockman, P. Burloct. J., Hess. O . V . , Bowen, F.W., RIAA Pap. No. 67-604, Sept. 1967

3. Connolly. D.J., Sovie, R.J., A I A A Pail. NO. 69-243, 'larch 1969

4. Experiments on current rotations in an MPD engine.

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. High-Power and High-Thrust-Density Electric Propulsion for In-Space Transportation;Nuclear Space Power and Propulsion Systems;2008-08-22

2. Numerical simulation of self-field MPD thrusters;27th Joint Propulsion Conference;1991-06-24

3. Geometric effects in applied-field MPD thrusters;21st International Electric Propulsion Conference;1990-07-18

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