{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,9,25]],"date-time":"2025-09-25T16:21:51Z","timestamp":1758817311593,"version":"3.37.3"},"reference-count":19,"publisher":"Springer Science and Business Media LLC","issue":"2","license":[{"start":{"date-parts":[[2024,1,24]],"date-time":"2024-01-24T00:00:00Z","timestamp":1706054400000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/creativecommons.org\/licenses\/by\/4.0"},{"start":{"date-parts":[[2024,1,24]],"date-time":"2024-01-24T00:00:00Z","timestamp":1706054400000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/creativecommons.org\/licenses\/by\/4.0"}],"funder":[{"name":"Funda\u00e7\u00e3o para a Ci\u00eancia e a Tecnologia","award":["UIDB\/50022\/2020","UIDB\/50022\/2020"],"award-info":[{"award-number":["UIDB\/50022\/2020","UIDB\/50022\/2020"]}]}],"content-domain":{"domain":["link.springer.com"],"crossmark-restriction":false},"short-container-title":["Int. J. Aeronaut. Space Sci."],"published-print":{"date-parts":[[2024,4]]},"abstract":"<jats:title>Abstract<\/jats:title><jats:p>In this article, the feasibility of spacecraft recovery using rotary wings is analysed. This technology possesses the ability to perform a safe and controlled landing, allowing the spacecraft to be reused and utilised in missions with different requirements. A computational model that simulates the descent of a sounding rocket was developed. It is based on rotor\u2019s aerodynamic theories and kinematics and computes several rotor parameters that allow the analysis of the system\u2019s performance. The model\u2019s verification was successfully carried out by comparing its behaviour with literature data. To understand how each design parameter influences the system, a parametric study of the rotor design variables was held. It was concluded that the blade\u2019s pitch angle is extremely important for the system\u2019s performance and should be carefully selected, and that weight penalties resultant from excessive blade\u2019s number or radius can be prejudicial. Furthermore, a design optimisation was conducted, aiming to minimise the rocket\u2019s terminal velocity. Finally, a flare manoeuvre was disclosed to reduce the touchdown velocity. This recovery system is concluded to be highly promising, though requiring further work in several fields of study.<\/jats:p>","DOI":"10.1007\/s42405-023-00696-z","type":"journal-article","created":{"date-parts":[[2024,1,24]],"date-time":"2024-01-24T10:02:19Z","timestamp":1706090539000},"page":"662-675","update-policy":"https:\/\/doi.org\/10.1007\/springer_crossmark_policy","source":"Crossref","is-referenced-by-count":2,"title":["Design of a Helicopter System Recovery for a Sounding Rocket"],"prefix":"10.1007","volume":"25","author":[{"given":"Jo\u00e3o Pedro Caldeira de Sousa","family":"Marques","sequence":"first","affiliation":[]},{"ORCID":"https:\/\/orcid.org\/0000-0001-7012-7320","authenticated-orcid":false,"given":"Alain","family":"de Souza","sequence":"additional","affiliation":[]},{"ORCID":"https:\/\/orcid.org\/0000-0003-1843-6120","authenticated-orcid":false,"given":"Filipe Szolnoky","family":"Cunha","sequence":"additional","affiliation":[]}],"member":"297","published-online":{"date-parts":[[2024,1,24]]},"reference":[{"key":"696_CR1","volume-title":"Coming home reentry and recovery from space","author":"RD Launius","year":"2012","unstructured":"Launius RD, Jenkins DR (2012) Coming home reentry and recovery from space, 1st edn. 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