Program of High Mach Integrated Control Experiment, “HIMICO” Using S-520 Sounding Rocket

Tetsuya SATO; Hideyuki TAGUCHI; Takayuki KOJIMA; Takeshi TSUCHIYA; Mitsuhiro TSUE; Shinji NAKAYA; Akiko MATSUO; Asei TEZUKA; Takahiro FUJIKAWA; Koji MIYAJI

doi:10.2322/tastj.19.831

Full Article

Program of High Mach Integrated Control Experiment, “HIMICO” Using S-520 Sounding Rocket

Tetsuya SATO, Hideyuki TAGUCHI, Takayuki KOJIMA, Takeshi TSUCHIYA, Mitsuhiro TSUE, Shinji NAKAYA, Akiko MATSUO, Asei TEZUKA, Takahiro FUJIKAWA, Koji MIYAJI

著者情報

Tetsuya SATO
Department of Applied Mechanics and Aerospace Engineering, Waseda University
Hideyuki TAGUCHI
Aeronautical Technology Directorate, Japan Aerospace Exploration Agency
Takayuki KOJIMA
Aeronautical Technology Directorate, Japan Aerospace Exploration Agency
Takeshi TSUCHIYA
Department of Aeronautics and Astronautics, The University of Tokyo
Mitsuhiro TSUE
Department of Aeronautics and Astronautics, The University of Tokyo
Shinji NAKAYA
Department of Aeronautics and Astronautics, The University of Tokyo
Akiko MATSUO
Department of Mechanical Engineering, Keio University
Asei TEZUKA
Department of Applied Mechanics and Aerospace Engineering, Waseda University
Takahiro FUJIKAWA
Department of Mechanical Engineering, Tokyo University of Science
Koji MIYAJI
Division of Systems Research, Yokohama National University

キーワード: Hypersonic Flight Test, HIMICO, Sounding Rocket, Airframe/Propulsion Integration

ジャーナルフリー

2021 年 19 巻 6 号 p. 831-837

DOI https://doi.org/10.2322/tastj.19.831

詳細

抄録

JAXA and some universities have proposed a hypersonic flight experiment named “HIMICO: High Mach Integrated Control Experiment” using a 1.5-meter class vehicle launched by the S-520 sounding rocket. The experiment aims to establish an integrated control method including the interference between the airframe and engine under the actual Mach 5 flight condition. Two flight experiments are planned step by step to reduce technical risks. Feasibility studies have been conducted by experiments and CFD analysis. This paper reports the summary of the flight test plan and preliminary studies on the vehicle shape, flight trajectory, component design and technical issues.

責任著者(Corresponding author)

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