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Ceyhun Tola
Ceyhun Tola
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Başlık
Alıntı yapanlar
Alıntı yapanlar
Yıl
Solid rocket motor propellant optimization with coupled internal ballistic–structural interaction approach
C Tola, M Nikbay
Journal of spacecraft and rockets 55 (4), 936-947, 2018
92018
Internal ballistic modeling of a solid rocket motor by analytical burnback analysis
C Tola, M Nikbay
Journal of Spacecraft and Rockets 56 (2), 498-516, 2019
82019
TURKSAT-3USAT: A 3U communication CubeSat with passive magnetic stabilization
AR Aslan, A Sofyali, E Umit, C Tola, I Öz, S Gülgönül
Proceedings of 5th International Conference on Recent Advances in Space …, 2011
82011
Mechanical design and finite element analysis of a 3 unit cubesat structure
C Güvenç, B Topcu, C Tola
Machines. Technologies. Materials. 12 (5), 193-196, 2018
52018
Investigation of the effect of thickness, taper ratio and aspect ratio on fin flutter velocity of a model rocket using response surface method
C Tola, M Nikbay
2015 7th International Conference on Recent Advances in Space Technologies …, 2015
42015
Effects of propellant properties on internal ballistic performance results of solid rocket motors
C Tola
Trans Motauto World 3 (4), 188-191, 2018
32018
Development of a 3Unit CubeSat for LEO Communication
AR ASLAN, B YAGCI, A SOFYALI, M SUER, E UMIT, C TOLA, O CEYLAN, ...
2nd Nano-Satellite Symposium, Tokyo University, Tokyo, Japan, 2011
32011
Preliminary Orbit Design for Turkish Regional Navigation Satellite System
S Büyük, ÖU Örengül, AC Başibüyük, U Tuğcular, TÇ Şişman, C Tola
2019 9th International Conference on Recent Advances in Space Technologies …, 2019
22019
Effects of Different Fin Shapes on Apogee and Stability of Model Rockets
A Pektaş, Z Demircan, Ü Hacıabdullahoğlu, N Ejder, C Tola
2019 9th International Conference on Recent Advances in Space Technologies …, 2019
22019
The Effect of Fiber Orientation Angle and Ply Thickness on Subsonic and Supersonic Flutter Characteristics of a Composite Missile Fin
C Tola, A Kayran
7th Ankara International Aerospace Conference, Ankara, Turkey, 2013
22013
TURKSAT-3USAT: A 3U Communication CubeSat
AR Aslan, A Sofyali, E Umit, C Tola, I Oz, S Gulgonul
The 3th Nano-satellite Symposium, 2011
22011
Solid rocket motor design using a surrogate model
C Tola, M Nikbay
Aircraft Engineering and Aerospace Technology 90 (7), 1104-1127, 2018
12018
Investigation of the Effects of Slotted Solid Propellant’s Sectional Geometry on Structural Strength and Internal Ballistic Performance of a Rocket Motor
C Tola, M Nikbay, M Methodologies, I Sonic
6th EASN International Conference on Innovation in European Aeronautics …, 2016
12016
Development of a Mechanical De-orbiting System for a 3-Unit CubeSat
C TOLA, AR ASLAN, M Ilarslan
3rd Nano-Satellite Symposium Japan 8 (6), 1, 2011
12011
Structural Behavior Examination of Frequently Used Solid Propellant Sections Under Centrifugal Loading Using Response Surface Method
C Tola, HB Eğlenoğlu
Journal of Aeronautics and Space Technologies 14 (2), 231-242, 2021
2021
Analysis of Range Extension Process for Outdated Ballistic Munitions Ejected from an Accelerator Launcher Concept J
C Tola, P Beyazpınar, D Akın
Aviat 5 (2), 90-100, 2021
2021
Türkiye Bölgesel Seyrüsefer Uydu Sisteminin Bir Artırım Sistemi Olarak Tasarımı ve Eniyilemesi
U Tuğcular, AC Başıbüyük, MF Engin, TÇ Şişman, C Tola, HE Söken
2020
Effects of Nozzle Throat and Combustion Chamber Design Variables on Divergent Portion of the Nozzle
N Önder, C Tola
2019 9th International Conference on Recent Advances in Space Technologies …, 2019
2019
Prediction of Cool-Down Time of a Solid Rocket Motor by a Surrogate Model
C Tola, M Nikbay
47th AIAA Thermophysics Conference, 4345, 2017
2017
Multidisciplinary Optimization of a Solid Propellant Sectional Geometry for Internal Ballistic and Structural Strength Criteria
C Tola, M Nikbay
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 5001, 2016
2016
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