Within the scope of this project, the objective is to design a critical safety system aimed at enhancing the safety and mission success of the KIZILELMA Unmanned Combat Aerial Vehicle (UCAV). Prospective candidates will develop a system that ensures the safe separation (jettisoning) of the Pylon Systems located at the underwing stations from the aircraft fuselage, either collectively or selectively at a specific weapon station, during emergency situations.

Through the implementation of this system, the risk of structural damage during takeoff or cruise will be minimized, safety risks associated with hung ordnance or improper launch will be prevented, potential fire and thermal hazards will be eliminated, and a direct contribution will be made to operational stealth (RF safety) by reducing the radar cross-section.

Criteria and Expectations

• The ability to design pylon mechanical integration interfaces that successfully meet the static and dynamic load limits for the heaviest munitions.
• Executing the design, alongside structural and dynamic analyses, of the spigot and tulip subsystems that facilitate safe separation (jettison).
• Delivering aerodynamic designs that maintain an optimal drag coefficient without disrupting the underwing airflow during flight.
• Constructing robust systems capable of satisfying operational and durability requirements under the high G-forces (UCAV acceleration conditions) generated during aircraft maneuvers.
• Conducting analytical studies regarding thermal expansion tolerances resulting from temperature fluctuations.
• Determining the appropriate surface treatments required to protect the system against severe environmental conditions, such as rain, icing, dust, and desert environments.

Relevant Academic Departments

• Mechanical Engineering
• Aeronautical Engineering
• Aerospace Engineering