{"id":22673,"date":"2025-10-22T15:00:13","date_gmt":"2025-10-22T15:00:13","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=22673"},"modified":"2025-10-22T15:00:13","modified_gmt":"2025-10-22T15:00:13","slug":"mach-5-propulsion-wind-tunnel-test-of-high-mach-integrated-control-experiment-aircraft-himico","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/10\/22\/mach-5-propulsion-wind-tunnel-test-of-high-mach-integrated-control-experiment-aircraft-himico\/","title":{"rendered":"Mach 5 Propulsion Wind Tunnel Test of High-Mach Integrated Control Experiment Aircraft (HIMICO)"},"content":{"rendered":"\n<p><strong>Hideyki TAGUCHI, Tetsuya SATO, Asei TEZUKA, Mitsuhiro TSUE, Takeshi TSUCHIYA, Shinji NAKAYA, Akiko MATSUO, Tomonari HIROTANI, Hidemi TAKAHASHI, Motoyuki HONGOH<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: HiSST-2025-233<\/strong><\/p>\n\n\n\n<p>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. <\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2025\/10\/HISST2025_233_paper.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Hideyki TAGUCHI, Tetsuya SATO, Asei TEZUKA, Mitsuhiro TSUE, Takeshi TSUCHIYA, Shinji NAKAYA, Akiko MATSUO, Tomonari HIROTANI, Hidemi TAKAHASHI, Motoyuki HONGOH<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: HiSST-2025-233<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,3362,3361],"tags":[1658,440,933],"class_list":["post-22673","post","type-post","status-publish","format-standard","hentry","category-events","category-high-speed-missions-and-vehicles-1-hisst-2025","category-1-hisst-2025","tag-air-breathing","tag-hypersonic","tag-propulsion","category-993","category-3362","category-3361","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/22673","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/comments?post=22673"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/22673\/revisions"}],"predecessor-version":[{"id":22675,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/22673\/revisions\/22675"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=22673"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=22673"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=22673"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}