YUMURTA
2024 — 2025 · Completed · Team Founder
A single-stage rocket developed from scratch with a 7-person team, reaching an apogee of XXX feet (XXX meters). We carried out a holistic design of the aerodynamic, structural and avionics subsystems to maximize flight stability and fly safely within transonic speed limits of Mach ~0.84. To analyze mechanical shocks in flight dynamics and test how far they can be reduced, rubber-based dampers were used for the payload, which is ejected at apogee and recovered independently. The system experimentally validates isolation performance by comparing data from IMU sensors in the damped and undamped zones.
Project Team
- Mehmet Orhan Şenaslan Advisor
- Canpolat Göregen Team Captain
- Mustafa Enes Yayla Mechanical Team Member
- Enes Pekdemir Mechanical Team Member
- Yunus Emre Çiftçi Avionics Team Member
- Yüksel Yurtbahar Avionics Team Member