Rocket engine altitude test facility design and 1D altitude simulation of IoX/LH2 propellant rocket engine
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2024
İSMAİL ÖZCAN
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DYNAMIC AND STRUCTURAL ANALYSIS OF ROCKET LAUNCH SYSTEMS
INTERNATIONAL GRADUATE RESEARCH SYMPOSIUM, İSTANBUL/TÜRKİYE, 1 Haziran 2022
ERGÜN FEYZA, OZKOL İBRAHİM, SEZENOĞLU FULİN, DEMİR ESRA
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Solid Rocket Motor Propellant Optimization with Coupled Internal Ballistic–Structural Interaction Approach
Journal of Spacecraft and Rockets, Vol. 55, No. 4, Temmuz 2018, s. 936-947, ISSN: 0022-4650
TOLA CEYHUN,NİKBAY MELİKE
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Internal Ballistic Modeling of a Solid Rocket Motor by Analytical Burnback Analysis
Journal of Spacecraft and Rockets, Vol. 56, No. 2, Mart 2019, s. 498-516, ISSN: 0022-4650
TOLA CEYHUN,NİKBAY MELİKE
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Hybrid Rocket Nozzle Erosion with Microaluminum-Added Fuel
Journal of Propulsion and Power, Vol. 38, Kasım 2022, ISSN: 2022-08-23
KARAKAŞ HAKKI, KAHRAMAN BÜŞRA, OZKOL İBRAHİM, KARABEYOĞLU MUSTAFA ARİF
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Performance evaluatıon of a staged combustıon cycle lıquıd rocket engıne rs-25 usıng a dıgıtal twın approach ın sıemens amesım
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2025
YASİR ŞİMES
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Optimal solution of orbital facility location problem utilizing optimum rocket staging and Q-Law orbit transfer
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2025
HASAN HÜSEYİN ÇAM
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Development of novel hybrid rocket internal ballistic configuration for in-space applications
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2022
MEHMET KAHRAMAN
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High temperature driven optimization of a hybrid rocket graphite nozzle design
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2024
ŞULE ÖZTÜRK
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Supersonic jet-wall interactions in model rocket launchers
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 1998
METİN UÇAK
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Supersonic impulse turbine design and optimization for liquid rocket engines
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2025
ANIL KÜÇÜK
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Assessment and optimization of a hybrid rocket motor as the final stage of small satellite launch vehicle
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2024
UKTE AKSEN
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Design and optimization of two stage launch vehicles with the same liquid propellant rocket engines in both stages
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2022
KUBİLAY ÖZÇELİK
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Pressure regulator design for liquid propellant rocket engines
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
ÇAĞRI İNANÇ
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Preliminary design tool for hybrid rocket engine powered leo nanosat launch vehicle and its application
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2019
NAZMİ ERDİ COŞKUNPINAR
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A mathematical model for prediction of film cooling performance in liquid propellant rocket engines
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
AKIN SÖZERİ
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Development of a Design and Performance Evaluation Code of Hybrid Rocket Motors
Asian Joint Conference on Propulsion and Power, 16 Mart 2016
COSKUNPINAR ERDİ,ÖZEN KAAN,GRATE STANISLAV,ASLAN ALİM RÜSTEM
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Prediction of Cool-Down Time of a Solid Rocket Motor by a Surrogate Model
AIAA Aviation and Aeronautics Forum and Exposition, Denver/AMERİKA BİRLEŞİK DEVLETLERİ, 5 Haziran 2017
TOLA CEYHUN,NİKBAY MELİKE
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Investigation of the Effects of Slotted Solid Propellant s Sectional Geometry on Structural Strength and Internal Ballistic Performance of a Rocket Motor
6th EASN International Conference on Innovation in European Aeronautics Research, porto/PORTEKİZ, 18 Ekim 2016
TOLA CEYHUN,NİKBAY MELİKE
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Investigation of the Effect of Thickness Taper Ratio and Aspect Ratio on Fin Flutter Velocity of a Model Rocket using Response Surface Method
7th International Conferenceon Recent Advances in Space Technologies, Istanbul/TÜRKİYE, 16 Haziran 2015
CEYHUN TOLA,NİKBAY MELİKE
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