Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Flight Path and Attitude

Hiroaki Watanabe; Koichi Matsuyama; Ken Matsuoka; Akira Kawasaki; Noboru Itouyama; Keisuke Goto; Kazuki Ishihara; Valentin Buyakofu; Tomoyuki Noda; Shiro Ito; Jiro Kasahara; Akiko Matsuo; Ikkoh Funaki; Daisuke Nakata; Masaharu Uchiumi; Hiroto Habu; Shinsuke Takeuchi; Satoshi Arakawa; Junichi Masuda; Kenzi Maehara; Tatsuro Nakao; Kazuhiko Yamada

doi:10.2514/6.2022-0231

Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Flight Path and Attitude

Hiroaki Watanabe, Koichi Matsuyama, Ken Matsuoka, Akira Kawasaki, Noboru Itouyama, Keisuke Goto, Kazuki Ishihara, Valentin Buyakofu, Tomoyuki Noda, Shiro Ito, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda, Kenzi MaeharaTatsuro Nakao, Kazuhiko Yamada

機械工学科

研究成果: Conference contribution

6 被引用数 (Scopus)

本文言語	English
ホスト出版物のタイトル	AIAA SciTech Forum 2022
出版社	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN（印刷版）	9781624106316
DOI	https://doi.org/10.2514/6.2022-0231
出版ステータス	Published - 2022
イベント	AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 - San Diego, United States 継続期間: 2022 1月 3 → 2022 1月 7

出版物シリーズ

名前	AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022

Conference

Conference	AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
国/地域	United States
City	San Diego
Period	22/1/3 → 22/1/7

ASJC Scopus subject areas

航空宇宙工学

文献へのアクセス

10.2514/6.2022-0231

他のファイルとリンク

引用スタイル

Watanabe, H., Matsuyama, K., Matsuoka, K., Kawasaki, A., Itouyama, N., Goto, K., Ishihara, K., Buyakofu, V., Noda, T., Ito, S., Kasahara, J., Matsuo, A., Funaki, I., Nakata, D., Uchiumi, M., Habu, H., Takeuchi, S., Arakawa, S., Masuda, J., ... Yamada, K. (2022). Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Flight Path and Attitude. In AIAA SciTech Forum 2022 [AIAA 2022-0231] (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2022-0231

Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31 : Flight Path and Attitude. / Watanabe, Hiroaki; Matsuyama, Koichi; Matsuoka, Ken その他.

AIAA SciTech Forum 2022. American Institute of Aeronautics and Astronautics Inc, AIAA, 2022. AIAA 2022-0231 (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).

研究成果: Conference contribution

Watanabe, H, Matsuyama, K, Matsuoka, K, Kawasaki, A, Itouyama, N, Goto, K, Ishihara, K, Buyakofu, V, Noda, T, Ito, S, Kasahara, J, Matsuo, A, Funaki, I, Nakata, D, Uchiumi, M, Habu, H, Takeuchi, S, Arakawa, S, Masuda, J, Maehara, K, Nakao, T & Yamada, K 2022, Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Flight Path and Attitude. in AIAA SciTech Forum 2022., AIAA 2022-0231, AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022, American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022, San Diego, United States, 22/1/3. https://doi.org/10.2514/6.2022-0231

Watanabe H, Matsuyama K, Matsuoka K, Kawasaki A, Itouyama N, Goto K その他. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Flight Path and Attitude. In AIAA SciTech Forum 2022. American Institute of Aeronautics and Astronautics Inc, AIAA. 2022. AIAA 2022-0231. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022). doi: 10.2514/6.2022-0231

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title = "Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Flight Path and Attitude",

author = "Hiroaki Watanabe and Koichi Matsuyama and Ken Matsuoka and Akira Kawasaki and Noboru Itouyama and Keisuke Goto and Kazuki Ishihara and Valentin Buyakofu and Tomoyuki Noda and Shiro Ito and Jiro Kasahara and Akiko Matsuo and Ikkoh Funaki and Daisuke Nakata and Masaharu Uchiumi and Hiroto Habu and Shinsuke Takeuchi and Satoshi Arakawa and Junichi Masuda and Kenzi Maehara and Tatsuro Nakao and Kazuhiko Yamada",

note = "Funding Information: This research was partially supported by Research-and-Development Grant Program (Engineering) in Institute of Space and Astronautical Science (ISAS) at Japan Aerospace Exploration Agency (JAXA) and Japan Society for the Promotion of Science (JSPS) KAKENHI (grant numbers 19H05464). The detonation engine system was designed and fabricated with the participation of NETS Inc., Yamamoto Machinery Design Co., Kawasho Design Co., Meiji Electric Industries Co., Ltd. The authors thank Dr. Kazuyuki Higashino, Prof. Takuma Endo, and Prof. Kazuhiro Ishii for fruitful discussion. The authors also thank other present or former laboratory members for their contribution to this project: Yuichi Kato, Junpei Nishimura, Takato Ukai, Koyo Kikuchi, Haruna Taki, Yuki Hayamizu, Junichi Higashi, Taihei Yamada, Tomoya Inakawa, Akiya Kubota, Toshiki Daicho, Koutaro Hotta, Masato Yamaguchi, Shun Watanabe, Motomu Asahara, Masaya Tanaka, Ryuya Yokoo, Juhoe Kim, Yuki Akimoto, Tomoyuki Sato, Satoru Sawada, Shiro Ito, Kose Ota, Kentaro Yoneyama, Yuse Kikuchi, Tomoaki Kimura, Kotaro Nakata, Karin Hattori, and Shinnichi Sugiura at Nagoya University and Tomoyuki Takano, Koki Arimatsu, Kasumi Hayashi, Keisuke Ikeda, Satoshi Inazumi, Kenta Mori, Genta Sugahara, Masaya Sumiyoshi, Hiromitsu Yagihashi, and Kazuki Yasuda at Muroran Institute of Technology. Funding Information: This research was partially supported by Research-and-Development Grant Program (Engineering) in Institute of Space and Astronautical Science (ISAS) at Japan Aerospace Exploration Agency (JAXA) and Japan Society for the Promotion of Science (JSPS) KAKENHI (grant numbers 19H05464). The detonation engine system was designed and fabricated with the participation of NETS Inc., Yamamoto Machinery Design Co., Kawasho Design Co., Meiji Electric Industries Co., Ltd. The authors thank Dr. Kazuyuki Higashino, Prof. Takuma Endo, and Prof. Kazuhiro Ishii for fruitful discussion. The authors also thank other present or former laboratory members for their contribution to this project: Yuichi Kato, Junpei Nishimura, Takato Ukai, Koyo Kikuchi, Haruna Taki, Yuki Hayamizu, Junichi Higashi, Taihei Yamada, Tomoya Inakawa, Akiya Kubota, Toshiki Daicho, Koutaro Hotta, Masato Yamaguchi, Shun Watanabe, Motomu Asahara, Masaya Tanaka, Ryuya Yokoo, Juhoe Kim, Yuki Akimoto, Tomoyuki Sato, Satoru Sawada, Shiro Ito, Kose Ota, Kentaro Yoneyama, Yuse Kikuchi, Tomoaki Kimura, Kotaro Nakata, Karin Hattori, and; AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 ; Conference date: 03-01-2022 Through 07-01-2022",

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T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022

AU - Watanabe, Hiroaki

AU - Matsuyama, Koichi

AU - Matsuoka, Ken

AU - Kawasaki, Akira

AU - Itouyama, Noboru

AU - Goto, Keisuke

AU - Ishihara, Kazuki

AU - Buyakofu, Valentin

AU - Noda, Tomoyuki

AU - Ito, Shiro

AU - Kasahara, Jiro

AU - Matsuo, Akiko

AU - Funaki, Ikkoh

AU - Nakata, Daisuke

AU - Uchiumi, Masaharu

AU - Habu, Hiroto

AU - Takeuchi, Shinsuke

AU - Arakawa, Satoshi

AU - Masuda, Junichi

AU - Maehara, Kenzi

AU - Nakao, Tatsuro

AU - Yamada, Kazuhiko

N1 - Funding Information: This research was partially supported by Research-and-Development Grant Program (Engineering) in Institute of Space and Astronautical Science (ISAS) at Japan Aerospace Exploration Agency (JAXA) and Japan Society for the Promotion of Science (JSPS) KAKENHI (grant numbers 19H05464). The detonation engine system was designed and fabricated with the participation of NETS Inc., Yamamoto Machinery Design Co., Kawasho Design Co., Meiji Electric Industries Co., Ltd. The authors thank Dr. Kazuyuki Higashino, Prof. Takuma Endo, and Prof. Kazuhiro Ishii for fruitful discussion. The authors also thank other present or former laboratory members for their contribution to this project: Yuichi Kato, Junpei Nishimura, Takato Ukai, Koyo Kikuchi, Haruna Taki, Yuki Hayamizu, Junichi Higashi, Taihei Yamada, Tomoya Inakawa, Akiya Kubota, Toshiki Daicho, Koutaro Hotta, Masato Yamaguchi, Shun Watanabe, Motomu Asahara, Masaya Tanaka, Ryuya Yokoo, Juhoe Kim, Yuki Akimoto, Tomoyuki Sato, Satoru Sawada, Shiro Ito, Kose Ota, Kentaro Yoneyama, Yuse Kikuchi, Tomoaki Kimura, Kotaro Nakata, Karin Hattori, and Shinnichi Sugiura at Nagoya University and Tomoyuki Takano, Koki Arimatsu, Kasumi Hayashi, Keisuke Ikeda, Satoshi Inazumi, Kenta Mori, Genta Sugahara, Masaya Sumiyoshi, Hiromitsu Yagihashi, and Kazuki Yasuda at Muroran Institute of Technology. Funding Information: This research was partially supported by Research-and-Development Grant Program (Engineering) in Institute of Space and Astronautical Science (ISAS) at Japan Aerospace Exploration Agency (JAXA) and Japan Society for the Promotion of Science (JSPS) KAKENHI (grant numbers 19H05464). The detonation engine system was designed and fabricated with the participation of NETS Inc., Yamamoto Machinery Design Co., Kawasho Design Co., Meiji Electric Industries Co., Ltd. The authors thank Dr. Kazuyuki Higashino, Prof. Takuma Endo, and Prof. Kazuhiro Ishii for fruitful discussion. The authors also thank other present or former laboratory members for their contribution to this project: Yuichi Kato, Junpei Nishimura, Takato Ukai, Koyo Kikuchi, Haruna Taki, Yuki Hayamizu, Junichi Higashi, Taihei Yamada, Tomoya Inakawa, Akiya Kubota, Toshiki Daicho, Koutaro Hotta, Masato Yamaguchi, Shun Watanabe, Motomu Asahara, Masaya Tanaka, Ryuya Yokoo, Juhoe Kim, Yuki Akimoto, Tomoyuki Sato, Satoru Sawada, Shiro Ito, Kose Ota, Kentaro Yoneyama, Yuse Kikuchi, Tomoaki Kimura, Kotaro Nakata, Karin Hattori, and

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PB - American Institute of Aeronautics and Astronautics Inc, AIAA

Y2 - 3 January 2022 through 7 January 2022

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