Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: History from Development to Flight

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

研究成果: Conference contribution

3 被引用数 (Scopus)

抄録

Detonation engines exert various characteristics and high propulsion performance depending on their operation modes. Our group has conducted the demonstration of the integrated RDE/PDE system (Detonation Engine System, DES) in outer-space environment using a sounding rocket named S-520-31 operated by Japan Aerospace Exploration Agency. This paper introduces the development history of DES from main integrity evaluations of preflight model to the outer-space demonstration of flight model.

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
ページ1-9
ページ数9
ISBN(印刷版)9781624106316
DOI
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 32022 1月 7

出版物シリーズ

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

Conference

ConferenceAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
国/地域United States
CitySan Diego
Period22/1/322/1/7

ASJC Scopus subject areas

  • 航空宇宙工学

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