Agni - 3
| Name | Agni-III |
|---|---|
| Image | |
| Country of origin | India (DRDO/BDL) |
| Type | Intermidiate range ballastic missile |
| Range | 3500-5000 km |
| Flight ceiling | >450 km |
| Length | 16.7 m |
| Diameter | 2.0 m |
| Mass | 48300 kg |
| Warhead | 1500 kg or 2490 kg (Claimed by two different sources) Conventional, thermobaric, strategic nuclear weapon |
| Max Speed | Not known |
| Propulsion | Solid fuel (Hydroxyl-terminated polybutadiene (HTPB)) |
| Engine | Dual stage solid rocket motor |
| Guidance | Mid-course: Ring laser gyroscope inertial navigation system, optionally augmented by GPS/NavIC satellite guidance Terminal: Imaging infrared homing, radar scene correlation, active radar homing. |
| Launch platform | 8 × 8 transporter erector launcher Rail mobile launcher |
| Service period | 2011-Present |
| Accuracy | 40 m CEP |
| Description | The Agni-III is an intermediate-range ballistic missile developed by India’s Defence Research and Development Organisation (DRDO). It has a range of 3,500 to 5,000 kilometers, allowing it to reach targets deep within neighboring countries. This two-stage, solid-fuel missile is highly mobile and can be launched from various platforms. Agni-III plays a crucial role in India’s nuclear deterrence strategy, providing a strong deterrent against potential adversaries. It incorporates advanced technologies such as a high-precision guidance system and a robust re-entry vehicle, ensuring its accuracy and survivability. The successful development and deployment of Agni-III have significantly enhanced India’s strategic capabilities and strengthened its position in the global strategic landscape. |
| Website | https://www.drdo.gov.in/ |
Disclaimer: This information is based on publicly available sources and should be considered for general knowledge purposes only.