Ukte Aksen | Aerospace | Best Researcher Award

Dr. Ukte Aksen | Aerospace | Best Researcher Award

Lead Engineer at Aselsan, Turkey

๐Ÿš€ Dr. Ukte Aksen is an aerospace engineer specializing in flight mechanics, aerodynamics, and hybrid rocket propulsion. He holds a PhD in Aerospace Engineering from Istanbul Technical University (ITU), where he researched hybrid rocket motors for small satellite launch vehicles. With experience at ASELSAN as a Lead Engineer, he previously worked at Milli Savunma รœniversitesi and Roketsan in guidance systems, flight dynamics, and simulation modeling. His expertise spans launch vehicle simulations, UAV dynamics, and hybrid propulsion. A CATIA, MATLAB/Simulink, and ANSYS expert, he has contributed to rocket and UAV projects. Fluent in English and German, he actively advances aerospace innovation. โœˆ๏ธ๐Ÿš€

Publication Profile

Scopus

Orcid

๐ŸŽ“ Educational Background

๐Ÿš€ Dr. Ukte Aksen earned his PhD in Aerospace Engineering from Istanbul Technical University (ITU) (2018-2024), focusing on the optimization of hybrid rocket motors for small satellite launch vehicles, under Prof. Dr. Alim Rรผstem Aslan. He completed his Masterโ€™s in Aerospace Engineering (2016-2018) at ITU, specializing in six-degree-of-freedom modeling and launch vehicle simulations. Dr. Aksen obtained his Bachelorโ€™s in Space Engineering (2011-2016) from ITU, ranking 2nd in his department. He attended รœskรผdar Ahmet KeleลŸoฤŸlu Anadolu High School (2007-2011), excelling in academics and achieving B1/C1 German proficiency. โœˆ๏ธ๐Ÿš€

๐Ÿ† Professional Experience

๐Ÿš€ Dr. Ukte Aksen is a Lead Engineer at ASELSAN (2022-present) in the Aerodynamics and Flight Dynamics Unit. Previously, he was a Research Assistant at National Defense University – Air Force Academy (2019-2022), specializing in flight mechanics and control. At ฤฐTรœNOVA TTO (2017-2019), he contributed to helicopter vibration reduction projects. He worked at Roketsan (2016-2017) in flight and orbital mechanics. His experience includes an internship at General Electric Aviation (2015) and Pegasus Airlines (2015). Early in his career, he gained customer service experience at LC Waikiki and LTB. His expertise spans aerospace systems, simulations, and propulsion technologies. โœˆ๏ธ๐Ÿš€

๐Ÿ’ป Technical Skills

Dr. Ukte Aksen possesses extensive expertise in engineering software and programming tools essential for aerospace applications. He is proficient in MATLAB/Simulink, Octave, and Scilab for computational modeling and simulation. His experience includes CATIA, UG/NX, and ANSYS for design and analysis, along with Hypermesh for advanced meshing. He is skilled in Datcom, RockSim, and XFLR5 for aerodynamic and flight simulations. Additionally, he has experience with C programming and MiniTab for statistical analysis. His knowledge extends to ArcGIS for geospatial applications, making him a versatile expert in aerospace engineering and computational analysis. ๐Ÿš€๐Ÿ’ก

๐Ÿš€ Research Focus

Dr. Ukte Aksen specializes in aerospace engineering, with a primary focus on trajectory design, optimization, flight dynamics, and space vehicle performance. His research includes six-degree-of-freedom trajectory modeling, multistage launch vehicle sensitivity analysis, and hybrid rocket propulsion. He also investigates geomagnetic storm effects on aviation safety and structural optimization of missile components. His expertise spans computational simulations, aerodynamics, and control systems for space applications. Through his contributions to Applied Sciences, Advances in Space Research, and Turkish Journal of Engineering, he advances aerospace technology and space mission design. ๐ŸŒ๐Ÿš€๐Ÿ“ก

Publication Top Notes

1๏ธโƒฃ Aksen, U. et al. (2024) โ€“ The effect of geomagnetic storms on aircraft accidents (1919โ€“2023) โ€“ Advances in Space Research, 73(1), 807-830 ๐ŸŒโœˆ๏ธ
2๏ธโƒฃ Aksen, U. et al. (2024) โ€“ Six-DOF Trajectory Optimization of a Launch Vehicle with Hybrid Last Stage (PSO Algorithm) โ€“ Applied Sciences, 14(9), 3891 ๐Ÿš€๐Ÿ“Š
3๏ธโƒฃ Aksen, U. et al. (2024) โ€“ Sensitivity Analysis Tool for Multistage Launch Vehicles โ€“ Turkish Journal of Engineering, 8(2), 254-264 ๐Ÿ“ˆ๐Ÿ›ฐ๏ธ
4๏ธโƒฃ Aksen, U. (2023) โ€“ Multi-Objective Geometric Optimization of a Missile Wing โ€“ Afyon Kocatepe Univ. Sci. & Eng. Journal ๐ŸŽฏ๐Ÿš€
5๏ธโƒฃ Aksen, U. (2022) โ€“ Effects of Wing Parameters on Glider Performance โ€“ IGRS, Istanbul โœˆ๏ธ๐Ÿ“‰
6๏ธโƒฃ Aksen, U. (2022) โ€“ Aeroelastic Analysis of SMA Modeled Wing Profile โ€“ UHUK, Izmir ๐Ÿ›ฉ๏ธ๐Ÿ”ฌ
7๏ธโƒฃ Aksen, U. (2022) โ€“ Impact of Wind Models on Glider Flight Dynamics โ€“ Savtek, Ankara ๐ŸŒฌ๏ธ๐Ÿ“Š
8๏ธโƒฃ Aksen, U. (2017) โ€“ Importance of Atmosphere Models in Aerospace Trajectory Simulation โ€“ AIAC, Ankara โ˜๏ธ๐Ÿš€
9๏ธโƒฃ Aksen, U. (2016) โ€“ FuegoSat: Real-Time Earth Observation Nano-Satellite Design โ€“ UHUK, Kocaeli ๐Ÿ›ฐ๏ธ๐ŸŒ