Agni-Prime | |
---|---|
Type | Medium-range ballistic missile |
Place of origin | India |
Service history | |
In service | Pre-induction Trials |
Used by | Strategic Forces Command |
Production history | |
Designer | Defence Research and Development Organisation |
Manufacturer | Bharat Dynamics Limited |
Specifications | |
Mass | 11,000 kg (24,000 lb) |
Length | 10.5 m (34 ft 5 in) |
Diameter | 1.15 m (3 ft 9 in) |
Warhead | 1x MaRV (or) 2x MIRV[1][2] (high explosive, thermobaric and nuclear) |
Warhead weight | 1,500 kg (3,300 lb) – 3,000 kg (6,600 lb) |
Engine | Two stage rocket motor with third stage MaRV[3][2] |
Propellant | Solid fuel |
Operational range | 1,000–2,000 kilometres (620–1,240 mi)[4] |
Guidance system | Ring laser gyro inertial navigation system with redundant micro inertial navigation and digital control system. Optionally augmented by GPS/NavIC satellite guidance.[5] |
Accuracy | <10 m CEP[6] |
Launch platform | Mobile rail-launcher Transporter erector launcher[4] |
Agni-Prime or Agni-P (Sanskrit: अग्नि; IAST: Agni; lit. Fire) is a two-stage, surface to surface, canister-launched, road mobile and solid-fueled medium-range ballistic missile being developed by India's Defence Research and Development Organisation (DRDO) as the sixth missile in the Agni series.[7] It is intended to be deployed in the operational service of the Strategic Forces Command, and to feature significant upgrades to the composite motor casing, a maneuverable reentry vehicle (MaRV) along with improved propellants, navigation and guidance systems.[8]
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