Shaurya | |
---|---|
Type | Short-range ballistic missile |
Place of origin | India |
Service history | |
Used by | Strategic Forces Command |
Production history | |
Designer | Research Centre Imarat (DRDO) |
Manufacturer | Bharat Dynamics Limited |
Produced | 2011–present |
Specifications | |
Mass | 6.2 t (6.8 short tons)[1] |
Length | 10 m (33 ft)[1][2] |
Diameter | 0.74 m (2.4 ft)[1] |
Warhead | Conventional and strategic nuclear weapon |
Warhead weight | 200–1,000 kilograms (440–2,200 lb) |
Engine | Two-stage solid rocket motor |
Propellant | Solid fuel |
Operational range | 700 to 800 km (430 to 500 mi)[3] |
Flight altitude | 50 km (31 mi) [1] |
Maximum speed | Mach 7.5 (9,190 km/h; 5,710 mph; 2.55 km/s)[1] |
Guidance system | Ring laser gyro inertial navigation system and accelerometer |
Accuracy | 20 m to 30 m CEP[4] |
Launch platform | Canisterised transporter erector launcher or underground silo[1] |
Shaurya (IAST: shāurya, meaning 'Bravery') is a canister-launched surface-to-surface short-range ballistic missile developed by the Indian Defence Research and Development Organisation (DRDO) for use by the Indian Armed Forces. It has a range of 700 to 800 km (430 to 500 mi) and is capable of carrying a payload of 200 to 1,000 kg (440 to 2,200 lb) conventional or nuclear warhead.[5]
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