An Experimental Study of an N<sub>2</sub>O / Ethanol Propulsion System with 2 kN Thrust Class BBM-Reference-Cited by-同舟云学术

An Experimental Study of an N₂O / Ethanol Propulsion System with 2 kN Thrust Class BBM

Published:2021 Issue:2 Volume:19 Page:186-192
ISSN:1884-0485
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
language:en
Short-container-title:AEROSPACE TECHNOLOGY JAPAN

Author:

TOKUDOME Shinichiro¹,YAGISHITA Tsuyoshi¹,GOTO Ken¹,SUZUKI Naohiro¹,YAMAMOTO Takayuki¹,DAIMOH Yasuhiro²

Affiliation:

1. Institute of Space and Astronautical Science, JAXA

2. IHI Aerospace Engineering

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/19/2/19_19.186/_pdf

Reference7 articles.

1. 1) Tokudome, S., Yagishita, T., Habu, H., Shimada, T., and Daimo, Y.: Experimental Study of an N2O/Ethanol Propulsion System, 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cincinnati, Ohio, AIAA Paper 2007-5464, 2007.

2. 2) Tokudome, S., Yagishita, T., Habu, H., Suzuki, N., Fukuyoshi, F., Goto, K., Daimo, Y., and Tamura, M.: Study of a Nitrous Oxide / Ethanol Propulsion System, 53rd Symposium on Space Science and Technology, Kyoto, Japan, 1B10, 2009 (in Japanese).

3. 3) Ordinance on Industrial Safety and Health Ministry of Labor Ordinance No. 34 of March 22, 2005, https://www.mhlw.go.jp/topics/bukyoku/iyaku/syokuten/dl/050322-1.pdf (in Japanese).

4. 4) Kawaguchi, J., Tokudome, S., Habu, H., Yagishita, T., and Chaen, S.: Thruster apparatus using nitrous oxide, Patent No. 4232820, December 19, 2008 (in Japanese).

5. 5) Sanuki, M.: Rocket Engineering, System of Mechanical Engineering No.32, Corona Publishing, Tokyo, 1981, pp. 51 (in Japanese).