Variant | TF-X |
Role | Multi-Role Fighter |
Country | Turkey |
Builder | SSB / TUSAS Türk Havacilik ve Uzay Sanayi |
First Flight | 2025 |
Status | development |
Number built | |
Operators | TuAF |
Cost | |
Comparable Aircraft | |
Recognition | |
Wingspan | 12 meters | 39 feet |
Sweep | |
Wing Aspect Ratio | |
Fuselage Maximum Diameter | meters | feet |
length | 19 meters | 60 feet |
height | meters | feet |
wing area | 60 sqm | 670 sqfeet |
Weight empty | kg | lb |
takeoff (clean) | kg | lb |
takeoff (maximum) | kg | 60,000 lb |
Fuel, Internal | kg | lb |
Fuel, External | kg | lb |
Payload | kg | lb |
Max weapon load | kg | lb |
Armament | |
Power Plant | |
Thrust, max, SLS, ISA | x kg | 2 x 20,000 lbst |
Internal fuel (usable) | kg | lb |
Performance (clean, ISA) | |
Max level speed (sea level) | KTAS |
Mach 2
Limit speed | KEAS / MN |
Stall speed (landing, 20% fuel) | 90 KCAS |
Stall speed (reference) | KCAS |
Rate of climb (SL) | feet/min |
Service ceiling | meters | +55,000 feet |
Combat Radius | km | + 600 nm |
Range / 3 ext. tanks (10% reserve) | km | nm |
Range, ext. tanks | 1111 km | nm |
Range, clean | km | nm |
Endurance, clean / ext. tanks | h min / hr |
Max sustained Load Factor (S.L.) | g |
Max sustained Load Factor (15,000 feet) | g |
Max sustained Turn Rate (15,000 feet) | deg/sec |
Takeoff ground run (S.L.) | meters | feet |
Landing ground roll (S.L., 20% internal fuel) | meters | feet |
Limit Load factor | + g / - g |
Crew | 1 |
Accomodations | |