Design, Fabrication and Testing of a Hybrid Rocket Engine Prototype

Authors

  • Dilara Koçak Mechanical Engineering Department,Faculty of Engineering, Ege University, İzmir - 35040, Türkiye https://orcid.org/0000-0002-0739-3447
  • Türker Erdem Öksüz Mechanical Engineering Department,Faculty of Engineering, Ege University, İzmir - 35040, Türkiye
  • Mertcan Koçak Mechatronics Engineering Department, Faculty of Engineering and Architecture, İzmir Katip Çelebi University, İzmir - 35620,
  • Utku Şentürk Mechanical Engineering Department,Faculty of Engineering, Ege University, İzmir - 35040, Türkiye
  • Necdet Özbalta Mechanical Engineering Department,Faculty of Engineering, Ege University, İzmir - 35040, Türkiye
  • Aydoğan Özdamar Mechanical Engineering Department,Faculty of Engineering, Ege University, İzmir - 35040, Türkiye

DOI:

https://doi.org/10.14429/dsj.74.19363

Keywords:

hybrid rocket, thrust, fabrication, experimental

Abstract

Rockets are generally used for defense purposes, for civilian purposes, for satellite launching and for orbiting and keeping the satellite in orbit. Chemical fuel rockets are examined in three groups as solid fuel rockets, liquid fuel rockets and hybrid fuel rockets. Due to the cost and complexity of liquid fuel rockets, the explosion hazard and thrust control problems of solid fuel rockets, studies on the use of hybrid rockets have recently become more common, considering the safety advantage. In this study, the thrust-time change was determined for the PVC..................

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Published

2024-11-25

How to Cite

Dilara Koçak, Türker Erdem Öksüz, Koçak, M., Şentürk, U., Özbalta, N., & Özdamar, A. (2024). Design, Fabrication and Testing of a Hybrid Rocket Engine Prototype. Defence Science Journal, 74(6), 942–949. https://doi.org/10.14429/dsj.74.19363

Issue

Vol. 74 No. 6 (2024)

Section

Missile Systems

License

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