Quick facts Agni-I/Agni-II/Agni-III/Agni-V, ನಮೂನೆ ...
| Agni-I/Agni-II/Agni-III/Agni-V |
Agni-II MRBM (Medium range ballistic missiles) |
| ನಮೂನೆ |
Medium Range Ballistic Missile (Agni-I)
Intermediate Range Ballistic Missile (Agni-II, Agni-III)
Intercontinental Ballistic Missile (Agni-V) |
| ಮೂಲ ಸ್ಥಳ |
India |
| ಕಾರ್ಯನಿರ್ವಹಣಾ ಇತಿಹಾಸ |
| ಸೇವೆಯಲ್ಲಿ |
(Tests) 04/11/99, 01/17/01 and 08/29/04 |
| ನಿರ್ಮಾಣ ಇತಿಹಾಸ |
| ನಿರ್ಮಾರ್ತೃ |
Defence Research and Development Organisation (DRDO), Bharat Dynamics Limited (BDL) |
| ಘಟಕ ವೆಚ್ಚ |
Rs 250-350 million (INR) or $ 5.6-7.9 million (USD) |
| ವಿವರಗಳು |
| ಭಾರ |
12,000 kg (Agni-I)
16,000 kg (Agni-II) |
| ಉದ್ದ |
15 m (Agni-I)
20 m (Agni-II)
16 m (Agni-III) |
| ವ್ಯಾಸ |
1.0 m (Agni-I, Agni-II)
2.0 m (Agni-III) |
|
| ಸಿಡಿತಲೆ |
Strategic nuclear (15 KT to 250 KT), conventional HE-unitary, penetration, sub-munitions, incendiary or fuel air explosives |
|
| ಎಂಜಿನ್ |
Single Stage (Agni-I)
Two-and-half-stage (Agni-II)
Two stage (Agni-III) solid propellant engine
|
| ಕಾರ್ಯವ್ಯಾಪ್ತಿ |
700 km (Agni-I)
2500 km (Agni-II)
3500 km (Agni-III)
5000-6000 km (Agni-V) |
| ಉಡ್ಡಯನದ ಎತ್ತರ |
> 90 km |
| ವೇಗ |
5-6 km/s (Agni-II) |
ಮಾರ್ಗದರ್ಶಕ
ವ್ಯವಸ್ಥೆ |
Ring Laser Gyro- INS (Inertial Navigation System), optionally augmented by GPS terminal guidance with possible radar scene correlation |
| ಉಡ್ಡಯನ ನೌಕೆ |
8 x 8 Tatra TELAR (Transporter erector launcher) Rail Mobile Launcher |
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