ÇAKIR

Country: Turkey
Company: Roketsan
Estimated price:
Not publicly disclosed
Maximum speed:
Mach 0,75–0,85
Flight altitude:
7,000 m
Maximum range:
150+ km
Warhead payload:
70 kg
Diameter:
Up to 275 mm
Launch weight:
Up to 330 kg

Other features: The missile accommodates multiple warhead options – including high-explosive, semi-piercing, blast-fragmentation, and thermobaric variants – and is powered by a turbojet engine supported by a solid-fuel launch booster. Its guidance and navigation suite features an inertial navigation system, anti-jam global navigation satellite system, radar and barometric altimeters, and a terrain-referenced navigation system for mid-phase flight, paired with imaging infrared, radio frequency, or hybrid imaging infrared and radio frequency seekers for terminal guidance. Engineered for multi-domain deployment, the system is compatible with fixed- and rotary-wing aircraft, unmanned combat aerial vehicles, autonomous surface vessels, tactical wheeled land vehicles, and surface platforms.