{"id":16489,"date":"2024-04-26T14:47:50","date_gmt":"2024-04-26T14:47:50","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16489"},"modified":"2024-04-26T14:47:51","modified_gmt":"2024-04-26T14:47:51","slug":"mission-engineering-for-space-rider","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/26\/mission-engineering-for-space-rider\/","title":{"rendered":"Mission Engineering for Space Rider"},"content":{"rendered":"\n<p><strong>Gabriele De Zaiacomo, Irene Pontijas Fuentes, Federico Trovarelli, Giovanni Medici, Cristina Recupero<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-188<\/strong><\/p>\n\n\n\n<p>The ESA Space Rider program aims at providing Europe with an affordable, independent, reusable endto-end integrated space transportation system, for routine access and return from low orbit. It will be<br>used to transport payloads for an array of applications, orbit altitudes and inclinations. The Space Rider<br>is composed of an expendable AVUM Orbital Module (AOM) and of a reusable Reentry Module (RM),<br>which is designed to be flown multiple times. For the RM this translates into the need for a flexible and<br>robust system, able to cope with a wide range of flight conditions, in compliance to stringent safety<br>constraints in case of failure. This is a critical additional challenge for Europe, beyond the current state<br>of the art in re-entry technology represented by the successful flight of the ESA IXV (Intermediate<br>eXperimental Vehicle) on February, 11th, 2015.<br>This paper presents the current status of the Space Rider Mission and the Mission Engineering results<br>achieved by DEIMOS Space at the Critical Design Review (CDR). The Mission Engineering is a design<br>process that includes multiple activities in support to the mission and system design: from aerodynamics<br>and flying qualities aspects to End-to-End (de-orbiting to touchdown) reference trajectories<br>optimization, analysis of the vehicle flight capabilities during entry and under parafoil, assessment of<br>the mission performance through Monte Carlo simulation campaigns, and visibility and safety analyses<br>during all phases of the return mission.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-188.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-188.pdf\">Read the full paper > <\/a><\/p>\n\n\n\n<p><strong><br><\/strong><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Gabriele De Zaiacomo, Irene Pontijas Fuentes, Federico Trovarelli, Giovanni Medici, Cristina Recupero<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-188<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[1009,1006],"tags":[1400,571,1399,568,573],"class_list":["post-16489","post","type-post","status-publish","format-standard","hentry","category-high-speed-missions-and-vehicles-hisst-2022","category-hisst-2022","tag-atmospheric-flight","tag-flying-qualities","tag-hypersonic-entry","tag-mission-analysis","tag-space-rider","category-1009","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16489","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=16489"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16489\/revisions"}],"predecessor-version":[{"id":16490,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16489\/revisions\/16490"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16489"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16489"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16489"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}