Fuel Regression Characteristics of Cascaded Multistage Impinging-Jet (CAMUI) Type Hybrid Rocket-Reference-Cited by-同舟云学术

Fuel Regression Characteristics of Cascaded Multistage Impinging-Jet (CAMUI) Type Hybrid Rocket

Published:2007 Issue:646 Volume:55 Page:516-526
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

Itoh Mitsunori,Maeda Takenori,Kakikura Akihito,Kaneko Yudai,Mori Kazuhiro,Nakashima Takuji,Wakita Masashi,Uematsu Tsutomu,Totani Tsuyoshi,Oshima Nobuyuki,Nagata Harunori

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/55/646/55_646_516/_pdf

Reference17 articles.

1. 1) Yuasa, S., Shimada, O., Imamura, T., Tamura, T. and Yamamoto, K.: A Technique for Improving the Performance of Hybrid Rocket Engines, AIAA Paper 99-2322, 1999.

2. 2) Yuasa, S., Yamamoto, K., Hachiya, H., Kitagawa, K. and Oowada, Y.: Development of a Small Sounding Hybrid Rocket with a Swirling-Oxidizer-Type Engine, AIAA Paper 2001-3537, 2001.

3. Heat transfer to impinging isothermal gas and flame jets

4. Flame impingement heat transfer: A review

5. A review of empirical flame impingement heat transfer correlations

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