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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Multidisciplinary Design Optimization of Reusable Launch Vehicles
23rd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, MONTREAL/KANADA, 10 Mart 2020
CUSİCK ANDREW, KONTİS KONSTANTİNOS, NİKBAY MELİKE
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Aerostructural Design Optimization Of High Speed Wings For Reusable Launch Vehicles
10th Ankara International Aerospace Conference (AIAC), 18 Eylül 2019
CUSİCK ANDREW,KONTİS KONSTANTİNOS,NİKBAY MELİKE
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Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams
ACTA MECHANICA, 2017, ISSN: 0001-5970
CİHAN MELAHAT,EKEN SEHER,KAYA METİN ORHAN
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Launch vehicle design, modeling and trajectory optimization
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2021
EMRE ÜNAL
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Brute force launch vehicle ascent trajectory assessment with a novel vectorized simulator
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2024
AHMET ENES YÜCEYURT
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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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Launch vehicle navigation system design and comprehensive performance analysis
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2024
ALTUĞ ERTAN
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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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The six degrees of freedom modeling and simulation of launch vehicles including sensitivity analysis
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2018
UKTE ÖNER
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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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Optimization of Allocation and Launch Conditions of Multiple Missiles for Three-Dimensional Collaborative Interception of Ballistic Targets
International Journal of Aerospace Engineering, Vol. 2016, Ocak 2016, s. 1-14, ISSN: 1687-5966
YUKSEK BURAK,ÜRE NAZIM KEMAL
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Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams
ACTA MECHANICA, Vol. 228, No. 12, Aralık 2017, s. 4353-4367, ISSN: 0001-5970
CİHAN MELAHAT, EKEN SEHER, KAYA METİN ORHAN
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Application of Linear Programming in Minimization of Campaign Launch Time of an GSM Operator
International Symposium of Production Research 2021, 7 Ekim 2021
CAMGÖZ AKDAĞ HATİCE, İSKENDER FATİH, KARAÇAYIR PINAR, ALAŞIK ASLI
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SharjahSat-1 Thermal Analysis for Orbit-Launch Selection
71ST International Astronautical Congress (IAC), CyberSpace Edition, 12 Ekim 2020
ALSABT İBRAHİM,ALKAABI TARIFA,MADARA SAHİTH REDDY,FERNİNİ ILYAS,KARABULUT BOGAC,ÇATAL EGEMEN,ALNAİMİY HAMİD M K,ASLAN ALİM RÜSTEM
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Dünya Birinciliği “Tasarla, Yap, Fırlat” (Annual CanSat Competition -Design Built Launch) Mikro Uydu Yarışması İTÜ UYARI Model Uydu Takımı
Amerikan Ulusal Havacılık ve Uzay Araştırmaları Merkezi (NASA), Amerikan Havacılık ve Uzay Enstitüsü (AIAA) ve Amerikan Astronomi Topluluğu (AAS), 2012
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