Conceptual Design Process of a Missile Model and Production Using Additive Manufacturing Method

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dc.contributor.authorAy, Nisa
dc.contributor.authorBozdemir, Mustafa
dc.date.accessioned2025-01-21T16:27:10Z
dc.date.available2025-01-21T16:27:10Z
dc.date.issued2024
dc.departmentKırıkkale Üniversitesi
dc.description.abstractThis study focuses on air-to-ground missile systems, which are widely used in Turkey and around the world and are becoming increasingly important. The development of missile systems takes into account various requirements defined by the end user. It is important to identify a system and its subcomponents that fully meet the requirements. This study analyzes an air-to-ground missile system and its main subcomponents identified through the conceptual design method based on the systematic design approach proposed by Pahl and Beitz. The aim is to determine the feasibility of obtaining an optimal solution that meets the requirements set by the conceptual design method. The missile design’s optimal solution was modeled using SolidWorks software. A three-dimensional (3D) printer with FDM production technology was used to produce a prototype of the computer-modeled design. ABS and ABS-plastic blend filaments were preferred due to their material properties in the FDM production process. During the printing stage, the filament and output settings of the model were determined using the 3D printer’s interface program. The filaments were then extruded through a nozzle, following the cross-sectional geometry of the part. The resulting model was printed in pieces and assembled with a tolerance of 0.1mm. This process resulted in a 3D model of the missile, which was created to represent the system structure in different colours. The study demonstrates that the conceptual design method can be used to develop innovative and meaningful missile models. © 2024, DESIDOC.
dc.description.sponsorshipKırıkkale Üniversitesi, KU, (2015/082)
dc.identifier.doi10.14429/dsj.74.19512
dc.identifier.endpage742
dc.identifier.issn0011-748X
dc.identifier.issue5
dc.identifier.scopus2-s2.0-85205147165
dc.identifier.scopusqualityQ2
dc.identifier.startpage734
dc.identifier.urihttps://doi.org/10.14429/dsj.74.19512
dc.identifier.urihttps://hdl.handle.net/20.500.12587/23282
dc.identifier.volume74
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherDefence Scientific Information and Documentation Centre
dc.relation.ispartofDefence Science Journal
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_20241229
dc.subject3D printer; Conceptual design; Systematic design; Weapon system
dc.titleConceptual Design Process of a Missile Model and Production Using Additive Manufacturing Method
dc.typeArticle

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