The TUK-F Launcher System is a pneumatic launch platform designed to safely and rapidly accelerate unmanned aerial vehicles (UAVs) or similar airborne platforms during takeoff. It is capable of launching vehicles with a takeoff weight between 20 kg and 100 kg, offering launch speeds between 10-35 m/s, adjustable based on platform weight. Its lightweight and modular structure allows for easy transport and quick deployment in the fıeld. With an integrated power system and electronic main control unit, it enables rapid setup and effıcient use under fıeld conditions.
TUK is designed as a versatile infrastructure offering a common solution for diverse-weight platforms and multi-scenario missions. Its development was guided by real field needs such as portability, short setıpn time, and adjustable speed.
Features such as portability, quick setup time, and adjustable launch speed have been developed in line with field-driven requirements.
TUK was conceived to replace bulky launch infrastructures with a lightweight yet effective alternative. Each unit is designed to be carried by two people and shipped in compact crates.
TUK ensures optimal launch pressure for UAVs with different weight categories.
The TUK project is not just a launch system - it is an innovative R&D platform pushing the limits of engineering.
Key engineering challenges addressed include:
With its unique design and analytical infrastructure, TUK leads the way for future R&D-based launcher systems in the defence industry.
System Components:
Application Areas: