{"id":16395,"date":"2024-04-24T12:41:10","date_gmt":"2024-04-24T12:41:10","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16395"},"modified":"2024-04-24T12:41:11","modified_gmt":"2024-04-24T12:41:11","slug":"experimental-measurements-on-teknaplasmasonic-high-enthalpyground-testing-facilities-using-350-kw-icpt-plasma-torch-to-reproduce-re-entry-conditions-of-space-vehicl","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/24\/experimental-measurements-on-teknaplasmasonic-high-enthalpyground-testing-facilities-using-350-kw-icpt-plasma-torch-to-reproduce-re-entry-conditions-of-space-vehicl\/","title":{"rendered":"Experimental measurements on Tekna\u2019\u2019PlasmaSonic\u2019\u2019 High EnthalpyGround Testing Facilities using 350 kW ICPT plasma torch to reproduce re-entry conditions of space vehicles"},"content":{"rendered":"\n<p><strong>Y. Lakaf, S. Xue<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-0404<\/strong><\/p>\n\n\n\n<p>This paper describes an experimental investigation of plasma jet properties on PlasmaSonic 350 kW Inductively<br>Coupled Plasma Tekna torch, operated in the Ground Testing Facility System, designed for thermal material<br>protection research and experimental studies of aerodynamics heating effect, under high enthalpy flow testing.<br>The ICPT-350 kW can be operated from 0.3 to 5 bar torch pressure and develops an enthalpy flow conditions<br>up to 31 MJ\/Kg. Various experimental measurements such us enthalpy, heat flux and sample surface<br>temperature are presented and discussed.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/04\/HiSST-2022-404.pdf\">Read the full paper here<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Y. Lakaf, S. Xue<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-0404<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[1006],"tags":[719,1295,744,1296],"class_list":["post-16395","post","type-post","status-publish","format-standard","hentry","category-hisst-2022","tag-high-enthalpy-flow","tag-intrusive-and-non-intrusive-techniques","tag-supersonic-flow","tag-tekna-icpt-350-kw","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16395","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=16395"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16395\/revisions"}],"predecessor-version":[{"id":16397,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16395\/revisions\/16397"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16395"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16395"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16395"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}