Competition
Mars Space Mission Design
Led an 11-member multidisciplinary team (İTÜ Team PYROEIS) for the 2024-2025 AIAA Undergraduate Team Space Design Competition. We designed a comprehensive Earth-to-Mars orbiter mission specifically tailored for atmospheric wind profiling.
Feb 2025 — Jun 2025
Mars Space Mission Design Presentation by Team PYROEIS
Advisor
Prof. Dr. Alim Rüstem AslanIstanbul Technical University - Project Advisor and Lecturer for the Spacecraft Systems Design II course.
Team Members
- Yunus SorgunçayTeam Captain
- Utku Sina TornacıDeputy Director
- Ömer Talha BaşoğluPayload & OBDH Coordinator
- Zeynep Şevval KaraPropulsion System Coordinator
- Muhammet Erdem AkbaşPropulsion System Coordinator
- Ozan YıldızGNC Coordinator
- Rahaf KatamechEPS Coordinator
- Hatice BilginStructure System Coordinator
- Özer Kaan KölemenoğluThermal Systems Coordinator
- Mirvari GuliyevaCommunication System Coordinator
- Salihcan SucuCommunication System Coordinator
Problem & Context
While previous missions provided insights into the Martian climate, comprehensive wind vector measurements in the lower Martian atmosphere are still lacking. Our challenge was to design a fully functional Mars orbiter within a $1 billion budget cap, integrated with a Doppler Wind LIDAR to capture spatial and seasonal wind dynamics, providing critical planning data for future Entry, Descent, and Landing (EDL) missions.
Accomplishments
- Coordinated an 11-member multi-disciplinary engineering team to design a complete mission architecture from launch to Mars orbit insertion (MOI).
- Integrated an adapted ALADIN Doppler Wind LIDAR instrument into the custom spacecraft bus design, balancing mass, thermal, power, and communication constraints.
- Conducted rigorous spacecraft subsystem-level trade studies, including AOCS (Attitude and Orbit Control System) sensor selection, thermal nodal analysis, and link budget calculations.
Gained Experience
- Developed strong leadership and project management skills while balancing performance, cost, and risk in a high-pressure environment.
- Gained hands-on expertise in systems engineering, mission architecture, and subsystem integration.
- Acquired the ability to translate scientific goals into actionable technical requirements and formal spacecraft documentation.
References
For additional references, please see the full project report.