Wind Tunnel Testing and Numerical Analysis on Angle-of-Attack 60º Side-Force Characteristics of Double-Cone Reusable Rocket-Reference-Cited by-同舟云学术

Wind Tunnel Testing and Numerical Analysis on Angle-of-Attack 60º Side-Force Characteristics of Double-Cone Reusable Rocket

Published:2022 Issue:1 Volume:70 Page:14-21
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

Takagi Yuya¹,Muto Tomotaro²,Kitamura Keiichi³,Nonaka Satoshi⁴

Affiliation:

1. 横浜国立大学大学院

2. 東京大学大学院

3. 横浜国立大学

4. 宇宙航空研究開発機構(ISAS/JAXA)

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

General Medicine

Link

https://www.jstage.jst.go.jp/article/jjsass/70/1/70_70_14/_pdf

Reference37 articles.

1. 1) Ogawa, H., Nonaka, S. and Inatani, Y.: A Concept and Its Aerodynamic Design of a Sub-Orbital Reusable Rocket, AIAA Paper 2004-2538, 2004.

2. 2) Ogawa, H., Nonaka, S., Naruo, Y., Ito, T. and Inatani, Y.: Reusable Sounding Rocket, Int. J. Microgravity Sci. Appl., 33 (2016), pp. 330303-1-330303-5.

3. 3) Nonaka, S., Nakamura, T., Ito, T. and Kamita, T.: Study on Flight Demonstration for Reusable Vehicle Experiment RV-X, 32nd International Symposium on Space Technology and Science, Fukui, Japan, 2019-g-01, 2019.

4. 4) Kimura, T., Hashimoto, T., Sato, M., Takada, S., Moriya, S., Yagishita, T., Naruo, Y., Ogawa, H., Ito, T., Obase, K. and Ohmura, H.: Reusable Rocket Engine: Firing Tests and Lifetime Analysis of Combustion Chamber, J. Propul. Power, 32 (2016), pp. 1087-1094.

5. 5) 中村隆宏，武藤智太朗，野中聡：再使用ロケット実験機RV-Xの空気力学，平成30年度宇宙航行の力学シンポジウム，相模原，2018.

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