{"id":16135,"date":"2024-04-12T10:11:11","date_gmt":"2024-04-12T10:11:11","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16135"},"modified":"2024-04-12T10:11:12","modified_gmt":"2024-04-12T10:11:12","slug":"space-rider-re-entry-module-gnc","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/12\/space-rider-re-entry-module-gnc\/","title":{"rendered":"Space Rider Re-Entry Module GNC"},"content":{"rendered":"\n<p><strong>J. Card\u00edn, F. Cacciatore, R. S\u00e1nchez, J. Veenman, G. Blanco, M. Lucrezia,C. Recupero, F. Tache, D. Bottero<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-98<\/strong><\/p>\n\n\n\n<p>Space Rider programme is devoted to providing Europe with and affordable, independent, reusable<br>end-to-end integrated space transportation system for routine access and return from low orbit,<br>operating in-orbit, de-orbiting, re-entering, landing on ground, being re-launched after limited<br>refurbishment. The Space Rider Re-Entry Module will be deorbited at the end of its operational mission,<br>it will separate from the AOM and carry out an orbital coasting and an atmospheric re-entry to<br>decelerate from hypersonic to supersonic speed. After that, the transonic regime is crossed during the<br>TAEM phase, followed by subsonic parachute deployment at Mach 0.73. At 5.5 km altitude the parafoil<br>is opened and the vehicle is steered towards the target landing site to execute a precision soft landing<br>within 150m accuracy. This paper describes the status of SR Re-Entry Module Guidance Navigation and<br>Control subsystem design, currently undergoing the overall System CDR<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-98.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-98.pdf\">Read the full paper > <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>J. Card\u00edn, F. Cacciatore, R. S\u00e1nchez, J. Veenman, G. Blanco, M. Lucrezia,C. Recupero, F. Tache, D. Bottero<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-98<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1007,1006],"tags":[576,1082,529,573],"class_list":["post-16135","post","type-post","status-publish","format-standard","hentry","category-events","category-guidance-control-systems-hisst-2022","category-hisst-2022","tag-gnc","tag-precision-landing","tag-re-entry","tag-space-rider","category-993","category-1007","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16135","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=16135"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16135\/revisions"}],"predecessor-version":[{"id":16136,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16135\/revisions\/16136"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16135"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16135"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16135"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}