Specifications:
Weight:
12,000 kg (Agni-I)
16,000 kg (Agni-II)
48,000 kg (Agni-III)
49,000 kg (Agni-V)
Length:
15 m (Agni-I)
21 m (Agni-II)
17 m (Agni-III)
17.5 m (Agni-V)
Diamete:
1.0 m (Agni-I, Agni-II)
2.0 m (Agni-III)
Type:
Medium-range ballistic missile (Agni-I)
Intermediate-range ballistic missile (Agni-II, Agni-III, Agni-IV)
Intercontinental ballistic missile (Agni-V)
Unit cost: #25 crore (US$4.99 million) to #35 crore (US$6.98 million) (Agni II)
Warhead Strategic nuclear (15 KT to
250 KT), conventional HE-unitary, penetration, sub-munitions, incendiary, or
fuel air explosives
Engine: Engine
Single stage (Agni-I)
Two-and-half-stage (Agni-II)
Two stage (Agni-III) solid propellant engine
Operational
Two-and-half-stage (Agni-II)
Two stage (Agni-III) solid propellant engine
Operational
range :
700-1,200 km (Agni-I)
2,000-3,500 km (Agni-II)
3,500-5,000 km (Agni-III)
Over 5,500 km (Agni-V)
Flight
altitude: 300 km (Agni-I)2,000-3,500 km (Agni-II)
3,500-5,000 km (Agni-III)
Over 5,500 km (Agni-V)
230 km (Agni-II),
350 km (Agni-III) Speed 2.5 km/s (Agni-I)
3.5 km/s (Agni-II)
Guidance system: Ring laser gyro-INS
internal navigation system, optionally augmented by GPS terminal guidance with possible radar scene correlation
Launch
platform: 8 x 8 Tatra TELAR (transporter erector luncher) rail mobile luncher
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