{"id":16147,"date":"2024-04-12T10:22:27","date_gmt":"2024-04-12T10:22:27","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16147"},"modified":"2024-04-12T10:22:28","modified_gmt":"2024-04-12T10:22:28","slug":"design-study-of-high-mach-integrated-control-experimental-aircraft-himico","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/12\/design-study-of-high-mach-integrated-control-experimental-aircraft-himico\/","title":{"rendered":"Design Study of High Mach Integrated Control Experimental Aircraft (HIMICO)"},"content":{"rendered":"\n<p><strong>Hideyuki Taguchi, Tomonari Hirotani, Tetsuya Sato, Asei Tzuka, Takeshi Tsuchiya and Takahiro Fujikawa<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-131<\/strong><\/p>\n\n\n\n<p>The design of High Mach Integrated Control Experimental aircraft (HIMICO) for the 1st flight experiment<br>has been progressed. The experiment aims to establish the design method of separation device,<br>telecommunication devices, heat shield structure, and aerodynamic control devices. Length and weight<br>of the aircraft are 1.2 m and 30 kg, respectively. The preliminary studies have been conducted on the<br>aerodynamics, trajectory, and heat shield structure. The reference trajectory is defined with 24 second<br>of the hypersonic flight duration. Aerodynamic force coefficients have been obtained at a hypersonic<br>wind tunnel and CFD analyses. A separation mechanism and a heat shield structure has been studied.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-131.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-131.pdf\">Read the full paper > <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Hideyuki Taguchi, Tomonari Hirotani, Tetsuya Sato, Asei Tzuka, Takeshi Tsuchiya and Takahiro Fujikawa<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-131<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1009,1006],"tags":[766,1092,440,933],"class_list":["post-16147","post","type-post","status-publish","format-standard","hentry","category-events","category-high-speed-missions-and-vehicles-hisst-2022","category-hisst-2022","tag-aerodynamics","tag-control","tag-hypersonic","tag-propulsion","category-993","category-1009","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16147","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\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/comments?post=16147"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16147\/revisions"}],"predecessor-version":[{"id":16148,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16147\/revisions\/16148"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16147"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16147"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16147"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}