Electrical Architecture of the Recovery System of a High Powered Rocket with Payload

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dc.contributor.authorBakirci, Murat
dc.contributor.authorOzer, Muhammed Mirac
dc.date.accessioned2025-03-17T12:22:48Z
dc.date.available2025-03-17T12:22:48Z
dc.date.issued2022
dc.departmentTarsus Üniversitesi
dc.description4th International Congress on Human-Computer Interaction, Optimization and Robotic Applications, HORA 2022 -- 9 June 2022 through 11 June 2022 -- Ankara -- 180434
dc.description.abstractIn this study, a recovery system design is presented for a high-powered rocket, which can carry and place a payload that performs scientific value experiments up to any altitude, as well as recovering flight data, and providing safe recovery of both the rocket and the payload. Rescue systems were designed, individually tested and integrated as a dual deployment with the drogue parachute opening at the apogee and the main parachute opening at lower altitude. However, the presented system is a reusable recovery mechanism that reduces consumed materials and speeds up the preparation process. This design engineering builds an infrastructure to improve the system by making a positive contribution to future studies and eliminating the shortcomings of past studies with an overview of the advantages and disadvantages of various systems. © 2022 IEEE.
dc.identifier.doi10.1109/HORA55278.2022.9800024
dc.identifier.isbn978-166546835-0
dc.identifier.scopus2-s2.0-85133971706
dc.identifier.scopusqualityN/A
dc.identifier.urihttps://doi.org/10.1109/HORA55278.2022.9800024
dc.identifier.urihttps://hdl.handle.net/20.500.13099/1396
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherInstitute of Electrical and Electronics Engineers Inc.
dc.relation.ispartofHORA 2022 - 4th International Congress on Human-Computer Interaction, Optimization and Robotic Applications, Proceedings
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_Scopus_20250316
dc.subjectelectrical system design
dc.subjecthigh powered rocket
dc.subjectpayload deployment
dc.subjectrecovery system
dc.subjectseparation system
dc.titleElectrical Architecture of the Recovery System of a High Powered Rocket with Payload
dc.typeConference Object

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