Ceyhun Tola
Title
Cited by
Cited by
Year
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
62011
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
32015
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
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
22019
TURKSAT-3USAT: A 3U Communication CubeSat
AR Aslan, A Sofyali, E Umit, C Tola, I Oz, S Gulgonul
Proc. 3rd Nano-Satellite Symp., 2011
22011
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
12018
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
12018
EFFECTS OF PROPELLANT PROPERTIES ON INTERNAL BALLISTIC PERFORMANCE RESULTS OF SOLID ROCKET MOTORS
C Tola
Trans Motauto World 3 (4), 188-191, 2018
12018
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
12013
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
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
2019
Solid rocket motor design using a surrogate model
C Tola, M Nikbay
Aircraft Engineering and Aerospace Technology, 2018
2018
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
The Effect of Fiber Orientation Angle on Subsonic and Supersonic Flutter Characteristics of a Composite Missile Fin
C Tola, A Kayran
7th Ankara International Aerospace Conference-AIAC, 2013
2013
Serbest Akıma Dik Doğrultuda Salınım Yapan Kanat-Sabit Kuyruk Çiftinin Etrafındaki Akım Yapısının Deneysel Olarak İncelenmesi
C Tola
Fen Bilimleri Enstitüsü, 2012
2012
Experimental Investigation of Flow Structures Around a Plunging Wing-fixed Tail Couple Steady Flow
C Tola
İstanbul Teknik Üniversitesi Fen Bilimleri Enstitüsü, 2012
2012
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
2011
3 BİRİMLİK KÜP UYDULAR İÇİN YÖRÜNGEDEN DÜŞÜRME SİSTEMİ TASARIMI
AK Karaaslan, C Tola
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Articles 1–20