An integrated solution for space shuttle launching ramp

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dc.contributor.authorYucenur, G. Nilay
dc.contributor.authorSubasi, Anil Sezer
dc.date.accessioned2024-03-13T10:35:38Z
dc.date.available2024-03-13T10:35:38Z
dc.date.issued2019
dc.departmentİstanbul Beykent Üniversitesien_US
dc.description.abstractPurpose The purpose of this study is to select the most appropriate city in Turkey for space shuttle launching ramp. Design/methodology/approach In the proposed approach, an integrated methodology is used. The SWARA method is used in the first phase of the solution for determining criteria's importance weights. Based on the criteria weights obtained by the SWARA method, the WASPAS method is used for selecting the best alternative. Findings Mugla is selected for the most suitable city for the first space shuttle launching pad according to determined criteria and proposed model. Research limitations/implications - Although there are 81 cities in Turkey, 4 alternatives were selected for evaluation. It is possible to eliminate this limitation by the future studies with the implementation of proposed model to entire of Turkey. Practical implications - This proposed model can be used by the countries which want to have a new or first space shuttle launching ramp in the world. Originality/value Although some climatic conditions are pointed out on the location of the space shuttle launching ramp, in literature, there is not a comprehensive and detailed evaluation example as much as the model proposed in this study. Therefore, this study is the first in terms of the proposed model and applied techniques in the sectoral sense. In addition, the study is also a guide for solving the original model which is revealed in the selection of the most suitable alternative city for space shuttle launching ramp by different multi-criteria decision-making methods.en_US
dc.identifier.doi10.1108/AEAT-10-2018-0257
dc.identifier.endpage1057en_US
dc.identifier.issn1748-8842
dc.identifier.issn1758-4213
dc.identifier.issue7en_US
dc.identifier.scopus2-s2.0-85068169194en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.startpage1051en_US
dc.identifier.urihttps://doi.org/10.1108/AEAT-10-2018-0257
dc.identifier.urihttps://hdl.handle.net/20.500.12662/4522
dc.identifier.volume91en_US
dc.identifier.wosWOS:000481468700016en_US
dc.identifier.wosqualityQ4en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherEmerald Group Publishing Ltden_US
dc.relation.ispartofAircraft Engineering And Aerospace Technologyen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectMCDMen_US
dc.subjectWASPASen_US
dc.subjectSpace explorationen_US
dc.subjectSpace launching rampen_US
dc.subjectSWARAen_US
dc.titleAn integrated solution for space shuttle launching rampen_US
dc.typeArticleen_US

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