Hatf-VIII Ra'ad | |
---|---|
Type | ALCM |
Place of origin | Pakistan |
Service history | |
In service | 2012–Present |
Used by | Pakistan Air Force |
Production history | |
Designer | National Engineering & Scientific Commission (Guidance/controls) Air Weapons Complex (Warhead design/assembly) |
Designed | 1998–2007 |
Manufacturer | Air Weapons Complex |
Variants | Ra'ad II |
Specifications (Technical data) | |
Mass | 1,100 kg (2,400 lb) |
Length | 4.85 m (15.9 ft) |
Diameter | 0.50 m (20 in) |
Maximum firing range | 550 km (340 mi) |
Warhead | ICM/HE/NE |
Warhead weight | 450 kg (990 lb) |
Blast yield | 5 kilotons of TNT (21 TJ)—12 kilotons of TNT (50 TJ)[1] |
Engine | Turbojet |
Payload capacity | 450 kg (990 lb) |
Operational range | 350 km (220 mi)–550 km (340 mi) |
Flight altitude | Terrain-following |
Maximum speed | ≤0.8 Mach. (980 km/h (610 mph)) |
Guidance system | Inertial, Terminal |
Accuracy | 3.0 m (9.8 ft) CEP[2] |
Launch platform | F-16A/B, Mirage-IIIR |
Transport | Combat aircraft |
The Ra'ad (Urdu: رعد; lit. "Thunder"; Military designation: Hatf-VIII Ra'ad, Transl.: Target-8), is a subsonic, standoff air-launched cruise missile (ALCM) jointly designed and developed by the National Engineering & Scientific Commission (NESCOM) and Air Weapons Complex.
It is deployed in the military service of Pakistan Air Force as Hatf-VIII, and has provided Pakistan with aerial nuclear deterrence.: 388–389 [3]