The MMU Life Support System Project aims to establish a life support system within the flight control system for the 5th generation TF-x to be produced for the National Combat Aircraft (MMU). The life support system will fulfill three main functions:
• Protecting the crew from physiological disturbances caused by the change in barometric pressure and G-LoC,
• Providing qualified breathing conditions for the crew,
• Providing demisting and in-cab ventilation.
The MMU Life Support System Project aims to establish a life support system within the flight control system of the 5th generation TF-x aircraft designed for the National Combat Aircraft (MMU). Within the scope of the project, it is aimed to fulfill the 3 basic functions of the life support system: 1) Protecting the crew from physiological disturbances caused by barometric pressure and G-LoC (Limitation Due to Forced Movements) changes, 2) Providing qualified breathing conditions for the crew, 3) Demisting and in-cabin provide ventilation.
These functions are important for the MMU to maintain the health and safety of the crew during flight, provide adequate oxygen and ensure proper ventilation of the interior cabin. Within the scope of the project, the life support system is designed to perform these basic functions effectively.