Agni-I | |
---|---|
Type | Short Range Ballistic Missile[1] |
Place of origin | India |
Service history | |
In service | 1979[2]—present |
Used by | Strategic Forces Command |
Production history | |
Designer | Defence Research and Development Organisation |
Manufacturer | Bharat Dynamics Limited |
Unit cost | ₹25 crore (US$3.0 million) to ₹35 crore (US$4.2 million)[3] |
No. built | 70 (2017 est.)[4] |
Specifications | |
Mass | 12,000 kg[5][6][7] |
Length | 15 m[5][6][7] |
Diameter | 1.0 m[6][7] |
Warhead | Conventional high explosive-unitary, penetration, cluster munition, incendiary, thermobaric, strategic nuclear weapon |
Warhead weight | 1,000 kg (2,200 lb) - 2,500 kg (5,500 lb)[8] |
Engine | Single stage composite rocket motor[9] |
Propellant | Solid fuel |
Operational range | 700–1,200 km [5][6] |
Flight ceiling | 370 km[7] |
Maximum speed | 2.5 km/s (9000 km/h)[6] |
Guidance system | Mid-course: Ring laser gyro inertial navigation system. Optionally augmented by GPS/NavIC satellite guidance Terminal: Radar scene correlation |
Accuracy | 25 m CEP[10] |
Launch platform | 8 x 8 Tatra transporter erector launcher/rail mobile[11] |
Agni-I (Agni "Fire") is a short-range ballistic missile[1] that was developed by DRDO of India in the Integrated Guided Missile Development Program. It is a single-stage missile that was developed after the Kargil War to fill the gap between the 250 km (160-mile) range of the Prithvi-II missile and the 2,500 km (1,600-mile) range of the Agni-II. It was first launched from a road mobile launcher at Integrated Test Range (ITR), Wheeler Island, on 25 January 2002.[12] Less than 75 launchers are deployed.[13]
The Agni-I is an Indian short-range ballistic missile (SRBM) with a range of 700 km