Design and performance of liquid propellant pulsed plasma thruster-Reference-Cited by-同舟云学术

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Design and performance of liquid propellant pulsed plasma thruster

Published:2004-04 Issue:3-4 Volume:73 Page:419-425
ISSN:0042-207X
Container-title:Vacuum
language:en
Short-container-title:Vacuum

Author:

Kakami Akira,Koizumi Hiroyuki,Komurasaki Kimiya,Arakawa Yoshihiro

Publisher

Elsevier BV

Subject

Surfaces, Coatings and Films,Condensed Matter Physics,Instrumentation

Reference7 articles.

1. Pulsed Plasma Thruster

2. Guman J. AFAPL-TR-68-132. New York, United States of America: Fairchild Hiller Corp; 1968.

3. Effects of Propellant and Electrode Geometry on Pulsed Ablative Plasma Thruster Performance

4. Kakami A, et al. Proceedings of 23rd International Symposium on Space Technology and Science, 2002; ISTS 2002-b-15.

5. Physics of electric propulsion;Robert,1968

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