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 | 24 | 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 | 19 | 2018 |
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 | 11 | 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 | 9 | 2018 |
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 | 8 | 2015 |
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 | 8 | 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 | 6 | 2019 |
Solid rocket motor design using a surrogate model C Tola, M Nikbay Aircraft Engineering and Aerospace Technology 90 (7), 1104-1127, 2018 | 5 | 2018 |
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 | 4 | 2016 |
Effects of propellant properties on internal ballistic performance results of solid rocket motors C Tola Trans Motauto World 3 (4), 188-191, 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 |
Analysis of range extension process for outdated ballistic munitions ejected from an accelerator launcher concept C Tola, P Beyazpınar, D Akın Journal of Aviation 5 (2), 90-100, 2021 | 2 | 2021 |
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 | 2 | 2016 |
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 | 2 | 2013 |
TURKSAT-3USAT: A 3U Communication CubeSat AR Aslan, A Sofyali, E Umit, C Tola, I Oz, S Gulgonul Proc. 3rd Nano-Satellite Symp, 2011 | 2 | 2011 |
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 | 1 | 2019 |
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 | 1 | 2011 |
TÜRKIYE BOLGESEL SEYRÜSEFER UYDU SISTEMININ BIR ARTIRIM SISTEMI OLARAK TASARIMI VE ENIYILEMESI U Tugcular, AC Basıbüyük, MF Engin, TÇ Sisman, C Tola, HE Söken | 1 | |
Jenerik Katı Bir Füze Kanat Geometrisinin Doğal Frekans Değerlerinin Çok Amaçlı Geometrik Optimizasyonu C Tola, U Aksen Afyon Kocatepe Üniversitesi Fen Ve Mühendislik Bilimleri Dergisi 23 (5 …, 2023 | | 2023 |
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 |