Agni-IV

From Astra Kosh, the AlphaDefense encyclopedia · Category: Strategic Systems

Agni-IV is an intermediate-range ballistic missile developed by DRDO’s Advanced Systems Laboratory (Hyderabad) as a substantially upgraded variant originally referred to as “Agni-II Prime,” redesignated Agni-IV to reflect its materially improved range, guidance and re-entry technology over the earlier Agni-II.[1]

Design

Agni-IV is a two-stage, solid-fuelled missile incorporating composite rocket-motor casings, a modern ring-laser-gyroscope-based inertial navigation system, and advanced re-entry vehicle technology enabling more accurate delivery at extended range compared to earlier Agni variants. It is designed to carry a payload of roughly 1,000 kg out to distances of up to 4,000 km, positioning it as a key intermediate-range link between the shorter Agni-II/III and the longer-range Agni-V.[1]

Specifications

Type Two-stage, solid-fuel intermediate-range ballistic missile
Developer Advanced Systems Laboratory, DRDO
Length / Weight 20 m / 17,000 kg
Range ~4,000 km
Payload ~1,000 kg (nuclear-capable)
Guidance Ring-laser-gyroscope inertial navigation with advanced re-entry vehicle
User Strategic Forces Command, India

Sources

  1. Wikipedia / Missile Threat (CSIS), “Agni-IV.”