Oğuzhan Açıkgöz,Mehmet Demir,Mehmet Emin Çetin

  • Oğuzhan Açıkgöz: Necmettin Erbakan Üniversitesi Havacılık ve Uzay Bilimleri Fakültesi
  • Mehmet Demir: Necmettin Erbakan Üniversitesi Havacılık ve Uzay Bilimleri Fakültesi
  • Mehmet Emin Çetin: Necmettin Erbakan Üniversitesi Havacılık ve Uzay Bilimleri Fakültesi
  •  Year : 2023
  •  Vol : 2
  •  Issue : 2
  •  Page : 78-85
In this study, a model rocket is designed for given mission parameters. Also, it is explained how a rocket prototype is produced and what parameters are used in the design phase. The design parameters may vary completely for different tasks and requirement configurations. The objective of this paper is to explain the design steps and performance analyses of a model rocket prototype. The rocket is designed from the beginning with the goal of high apogee and a higher payload. Design steps and simulations are demonstrated, and rockets are manufactured by evaluating the optimization. Nose cone, fin, and material strength calculations in rockets are performed in detail to prevent the drawbacks of instabilities. The manufacturing of the model rocket, its design, and the simulation of the rocket prototype are successfully done.
Cite this Article As : Açıkgöz, O., Demir, M., & Çetin, M. E. (2023). Design and simulation of a model rocket prototype. Aerospace Research Letters (ASREL) Dergisi, 2(2), 78-85. http://dx.doi.org/10.56753/ASREL.2023.2.3

Conflict of interest : Yok

This article is published under the CC BY-NC 4.0 license.
Asrel Aerospace Research Letters
2023, Vol2, Issue2
E-ISSN: 2980-0064
Received : , Accepted : , Published Online :