Art

J-GLOBAL ID：200902212838599876   Reference number：06A0162036

Numerical Analysis of a Radiation-Cooled Micro Arcjet Thruster

放射冷却マイクロアークジェットスラスタの数値解析

Author (2)： OKAMOTO Hiroyuki (Astro Res. Corp., Yokohama, JPN) ,  NISHIDA Michio (Sojo Univ., Kumamoto, JPN)
Material： Transactions of the Japan Society for Aeronautical and Space Sciences  (Trans Jpn Soc Aeronaut Space Sci)
Volume： 48  Issue： 162  Page： 187-192  Publication year： Feb. 04, 2006 
JST Material Number： F0167A  ISSN： 0549-3811  CODEN： TJASA  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： ENGLISH (EN)

Thesaurus term： *internal flow ,...
Semi thesaurus term： *electric rocket engine ,...

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JST classification (1)： Rocket engines  (PB02050J)

Reference (6)：

• 1) Willmes, G. F. and Burton, R. L.: Low-Power Helium Pulsed Arcjet, J. Propul. Power, 15 (1999), pp. 440–446.
• 2) Ashiya, H., Horisawa, H. and Kimura, I.: Discharge Characteristics of a Very Low-Power Arcjet, 1G3, the 46th Space Sciences and Technology Conference, Tokyo, 2002 (in Japanese).
• 3) Bird, G. A.: Molecular Gas Dynamics and Direct Simulation of Gas Flows, Oxford University Press, New York, 1994.
• 4) Boyd, I. D.: Extensive Validation of Monte Carlo Method for Hydrogen Arcjet, J. Propul. Power, 13 (1997), pp. 775–782.
• 5) Martinez-Sanchez, M.: Simplified Analysis of Arcjet Operation, Lecture 11–12, 16.522 Space Propulsion, Aeronautics and Astronautics, Masachusetts Institute of Technology, 2004; URL http://ocw.mit.edu/NR/rdonlyres/Aeronautics-and-Astronautics/16-522Spring2004/030CF8D9-FFA9-41C3-B430-7E49311E6D6D/0/lecture11_12.pdf

Terms in the title (4)： 放射冷却 ,  マイクロ ,  アークジェットスラスタ ,  数値解析