{"id":16224,"date":"2024-04-12T12:52:00","date_gmt":"2024-04-12T12:52:00","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16224"},"modified":"2024-04-12T12:52:01","modified_gmt":"2024-04-12T12:52:01","slug":"sabre-bypass-ramjet-concept-evaluation-2","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/12\/sabre-bypass-ramjet-concept-evaluation-2\/","title":{"rendered":"SABRE Bypass Ramjet Concept Evaluation"},"content":{"rendered":"\n<p><strong>Christoph Bauer, Reinhold Baumann, Guido Kurth, Ralf Schlaps , Johan Steelant and Philipp<br>St\u00f6rchle<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-304<\/strong><\/p>\n\n\n\n<p>SABRE &#8211; Synergetic Air Breathing Rocket Engine \u2013 combines the advantages of a high specific impulse<br>air breathing engine with a high thrust\/weight ratio rocket motor. During air breathing mode, SABRE &#8211;<br>operating in a combined turbomachinery based cycle of the core engine and ramjet cycle of the bypass<br>burner &#8211; captures the ambient air as oxidizer [1]. To minimize drag, the adjustable air intake system is<br>capable of aligning the shock structure to the free stream Mach number and capturing the maximum<br>possible air mass flow.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-304.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-304.pdf\">Read the full paper > <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Christoph Bauer, Reinhold Baumann, Guido Kurth, Ralf Schlaps , Johan Steelant and Philipp<br \/>\nSt\u00f6rchle<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-304<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1006,1013],"tags":[451,967],"class_list":["post-16224","post","type-post","status-publish","format-standard","hentry","category-events","category-hisst-2022","category-propulsion-systems-and-components-hisst-2022","tag-ramjet","tag-sabre","category-993","category-1006","category-1013","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16224","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=16224"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16224\/revisions"}],"predecessor-version":[{"id":16225,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16224\/revisions\/16225"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16224"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16224"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16224"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}