| 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 | 7 | 2011 |
| 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 | 4 | 2015 |
| 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 | 3 | 2019 |
| 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 | 3 | 2018 |
| 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 | 3 | 2011 |
| 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 | 2 | 2019 |
| 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 | 2 | 2018 |
| TURKSAT-3USAT: A 3U Communication CubeSat AR Aslan, A Sofyali, E Umit, C Tola, I Oz, S Gulgonul The 3th Nano-satellite Symposium, 2011 | 2 | 2011 |
| Effects of propellant properties on internal ballistic performance results of solid rocket motors C Tola Trans Motauto World 3 (4), 188-191, 2018 | 1 | 2018 |
| 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 | 1 | 2013 |
| 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 | | |
