Hideyki TAGUCHI, Tetsuya SATO, Asei TEZUKA, Mitsuhiro TSUE, Takeshi TSUCHIYA, Shinji NAKAYA, Akiko MATSUO, Tomonari HIROTANI, Hidemi TAKAHASHI, Motoyuki HONGOH
DOI Number: N/A
Conference number: HiSST-2025-233
Research and development of the hypersonic integrated control experimental aircraft (HIMICO) was carried out with the aim of establishing elemental technologies for a hypersonic aircraft that flies at Mach 5. Hypersonic intake wind tunnel tests, hydrogen ramjet combustion tests, hypersonic aircraft aerodynamic tests, etc. were conducted to obtain elemental performance. A propulsion wind tunnel experiment simulating Mach 5 flight conditions is planned to confirm the heat-resistant aircraft structure and the function of the onboard equipment, and to evaluate the propulsive performance of the hypersonic engine mounted on the aircraft.