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Koç, Fatma Serra (2024) How does varying the nozzle diameter of a miniature rocket (2.6 cm, 2.8cm, 3.0cm, 3.2cm,3.4cm,3.6cm, 3.8cm) and the change in the fin angle (30, 40,50) between rocket body and wings affect the maximum altitude that the rocket can reach, and what is the nature of the relationship between nozzle diameter, fin angle and maximum altitude? Other thesis, TED Ankara Koleji.