TÜBİTAK 2209-B - ROKETSAN

Problem: During their missions, rocket systems are exposed to high levels of random vibration, shock and acoustic loads, which can cause critical failures in electronic boards, batteries and connectors. The conventional dampers used in the industry (such as metal springs or silicone mounts) are generally heavier, more expensive and require long procurement lead times.

Solution: In this project, an innovative, lightweight "print-and-fit" module was designed that can be tuned to the mission profile, using additive manufacturing (FDM/FFF) and TPU, a flexible material.

Testing and Validation: The project integrates mathematical, laboratory and real flight tests.

1. Numerical Analysis: Damper candidates are first examined with FEA-based simulations to predict their performance.
2. Ground Tests: 3D-printed prototypes are tested in the laboratory and the most suitable design is selected.
3. Flight Tests: The final design will be integrated into a model rocket launched at the Aksaray Hisar Test Center and validated under real conditions using in-flight telemetry and accelerometer data.