Parametric comparison of four different missile system

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dc.contributor.authorTopalömer, Mehmet
dc.contributor.authorGündoğan Türker, Çiğdem
dc.date.accessioned2025-02-09T14:34:55Z
dc.date.available2025-02-09T14:34:55Z
dc.date.issued2019
dc.departmentEnstitüler, Lisansüstü Eğitim Enstitüsü, Savunma Teknolojileri Ana Bilim Dalı
dc.departmentFakülteler, Mühendislik Fakültesi, Mekatronik Mühendisliği Bölümü
dc.description.abstractIn the design of a missile, the rocket engine, aerodynamics, structural warhead, fuse, launcher and control unit are important with the guidance system. Four different missiles named as Atgm_1, Low Drag_8, Patriot_TR, and New Missile are designed. The structure and working principle of the missiles are analized. The designed missiles were simulated at a platform with shooter and target values determined by the Rocket Simulator Program. Speed, distance, altitude, mach number and maneuverability number which are important criteria during the cruise, test flight or when the missiles take action to hit the target were evaluated by test flights in the simulation.
dc.identifier.endpage20
dc.identifier.issn2651-5199
dc.identifier.issn2822-7085
dc.identifier.issue2
dc.identifier.startpage15
dc.identifier.urihttps://hdl.handle.net/11501/1940
dc.identifier.urihttps://dergipark.org.tr/tr/pub/ijens/issue/62959/1006006
dc.identifier.volume2
dc.institutionauthorTopalömer, Mehmet
dc.institutionauthorGündoğan Türker, Çiğdem
dc.institutionauthorid0000-0003-0482-1810
dc.language.isoen
dc.publisherIstanbul Gedik University
dc.relation.ispartofInternational Journal of Engineering and Natural Sciences
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_DergiPark_20250209
dc.subjectDefence Technologies
dc.subjectDefence Industry
dc.subjectMissile Design
dc.subjectTest Flight
dc.titleParametric comparison of four different missile system
dc.typeArticle

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