{"id":16123,"date":"2024-04-12T09:58:40","date_gmt":"2024-04-12T09:58:40","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16123"},"modified":"2024-04-12T09:58:41","modified_gmt":"2024-04-12T09:58:41","slug":"space-rider-entry-and-taem-gc-of-the-future-european-reusable-space-transportation-system","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/12\/space-rider-entry-and-taem-gc-of-the-future-european-reusable-space-transportation-system\/","title":{"rendered":"SPACE RIDER: Entry and TAEM G&amp;C of the Future European Reusable Space Transportation System"},"content":{"rendered":"\n<p><strong>C. Recupero, A. Fabrizi, M. Kerr, G. De Zaiacomo, V. Fernandez, P. Rosa, A. Tarabic, A.Cojocaru, F. Tache, F. Cacciatore<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-77<\/strong><\/p>\n\n\n\n<p>This paper presents the Space Rider (SR) Entry and TAEM (Terminal Area Energy Management) G&amp;C,<br>at the closure of delta-CDR of the Space Rider ESA program. Space Rider is an ESA development<br>program that aims to provide Europe with an affordable, independent, reusable end-to-end integrated<br>space transportation system for routine access and return from low orbit. It will be used to transport<br>payloads for an array of applications, orbit altitudes and inclinations. The paper presents an overview<br>of the Entry and TAEM G&amp;C Design Definition and Justification, as carried out in the phase C of the<br>Space Rider program, with the Entry and TAEM G&amp;C designed to take the vehicle from hypersonic<br>conditions at the Entry Interface Point (EIP) (\uf07eVelocity 7.5km\/s, 120km) to subsonic conditions at the<br>parachute release (\uf07eMach 0.73, 16km). The paper provides information on a range of activities for the<br>Entry and TAEM G&amp;C, including: Entry and TAEM G&amp;C requirements evaluation and analysis, Entry and<br>TAEM G&amp;C concept, functional and physical architecture definition and justification, and the assessment<br>of the GNC performance through Monte Carlo simulation campaigns. Most of the Space Rider RM Entry<br>and TAEM Guidance and Control are based on the IXV algorithms. The promising simulation results<br>obtained demonstrate a high level of performance of the Entry and TAEM G&amp;C, as well as robustness<br>against conservative (enlarged) model uncertainties and mission parameters dispersion, providing a<br>solid basis for the Entry and TAEM G&amp;C in subsequent program phases.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-77.pdf\">Read the full paper > <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>C. Recupero, A. Fabrizi, M. Kerr, G. De Zaiacomo, V. Fernandez, P. Rosa, A. Tarabic, A.Cojocaru, F. Tache, F. Cacciatore<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-77<\/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":[576,529,573,577],"class_list":["post-16123","post","type-post","status-publish","format-standard","hentry","category-events","category-guidance-control-systems-hisst-2022","category-hisst-2022","tag-gnc","tag-re-entry","tag-space-rider","tag-taem","category-993","category-1007","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16123","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=16123"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16123\/revisions"}],"predecessor-version":[{"id":16124,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16123\/revisions\/16124"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16123"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16123"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16123"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}