| Agni-I/Agni-II/Agni-III/Agni-V |
|---|
Agni-II MRBM (Medium range ballistic missiles) |
| Type | Medium Range Ballistic Missile (Agni-I)
Intermediate Range Ballistic Missile (Agni-II, Agni-III)
Intercontinental Ballistic Missile (Agni-V) |
|---|
| Place of origin | India |
|---|
| Service history |
|---|
| In service | (Tests) 04/11/99, 01/17/01 and 08/29/04 |
|---|
| Production history |
|---|
| Manufacturer | Defence Research and Development Organisation (DRDO), Bharat Dynamics Limited (BDL) |
|---|
| Unit cost | Rs 250-350 million (INR) or $ 5.6-7.9 million (USD)[1] |
|---|
| Specifications |
|---|
| Weight | 12,000 kg (Agni-I)
16,000 kg (Agni-II)
55,000 kg (Agni-III)[2] |
|---|
| Length | 15 m (Agni-I)
20 m (Agni-II)
17 m (Agni-III)[2] |
|---|
| Diameter | 1.0 m (Agni-I, Agni-II)
2.0 m (Agni-III)[2] |
|---|
|
| Warhead | Strategic nuclear (15 KT to 250 KT), conventional HE-unitary, penetration, sub-munitions, incendiary or fuel air explosives |
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|
| Engine | Single Stage (Agni-I)
Two-and-half-stage (Agni-II)
Two stage (Agni-III) solid propellant engine
|
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Operational
range | 700-800 km (Agni-I)
2000-3500 km (Agni-II)
3500-5500 km (Agni-III)
5000-6000 km (Agni-V) |
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| Flight altitude | > 90 km |
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| Speed | 5-6 km/s (Agni-II)[3] |
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Guidance
system | Ring Laser Gyro- INS (Inertial Navigation System), optionally augmented by GPSterminal guidance with possible radar scene correlation |
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Launch
platform | 8 x 8 Tatra TELAR (Transporter erector launcher) Rail Mobile Launcher |
|---|
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