Saraçyakupoğlu, TamerÖzçelik, Ahmet DevletDelibaş, Heyzem Doğukan2022-05-122022-05-122022Saraçyakupoğlu T., Delibaş H. D., Özçelik A. D “An Experimental Determination and Numerical Analysis of A Loiter Munition Unmanned Aerial Vehicle System” Int. J. of 3D Printing Tech. Dig. Ind., 6(1): 83-101, (2022).2602-33502602-3350https://hdl.handle.net/11363/3502https://search.trdizin.gov.tr/tr/yayin/detay/514825https://doi.org/This paper experimentally determinates the calculation of an Unmanned Aerial Vehicle (UAV) and analyzes the design criteria within four different scenarios. The UAV to be designed is a loiter munition UAV system. A mobile or equipment such as a parachute and/or airbag. The UAV may be operable day and night conditions, capable of 2-3 hours of flight hours, and will be launched from a catapult. The UAV navigation system is compact and easily controlled by a personal Global Positioning System (GPS). The mentioned UAV will have a vast operational capability, especially for defense and border security activities since it is equipped with advanced avionics and a small physical footprint for covert operations. As a consequence of this research, it can be claimed that the UAV's mid-wing, twin-tail, and relatively light body will have three axis stability and offer numerous benefits, particularly in terms of operational cost.eninfo:eu-repo/semantics/openAccessAttribution-NonCommercial-NoDerivs 3.0 United StatesMission profileSpeed conditionWeight calculationArticle618310110.46519/ij3dptdi.1083686514825