Agni I Missile
Agni-I is a single stage, solid fuel, road and rail mobile, medium-range ballistic missiles (MRBM) using solid propulsion upper stage, derived from Prithvi, essentially to prove the re-entry structure, control and guidance. The strap-down inertial navigation system adopts explicit guidance—attempted for the first time globally. Using carbon composite structure for protecting payload during its re-entry phase, the first flight was conducted in May 1989, thus establishing the re-entry technology and precise guidance to reach the specific targets. This shorter ranger missile is specially designed to strike targets in Pakistan.

Agni II is an operational version of Agni I and is an intermediate range ballistic missile (IRBM) with two solid fuel stages and a Post Boost Vehicle (PBV) integrated into the missile’s Reentry Vehicle (RV) with mobile launch capability test-fired in April 1999. The range for Agni II is more than 2000 km. Quick deployment of the Agni II was possible, by building on the earlier Agni-TD programme that provided proven critical technologies and designs required for long range ballistic missiles. The Agni II missile was last test fired in May 2009. A new variant of the Agni II called the Agni IIIA is presently under development.
Agni III Missile With 3,500 km
Additionally, Agni III, an intermediate-range ballistic missile was developed by India as the successor to Agni II. Intended to be a two-stage ballistic missile capable of nuclear weapons delivery, it is touted as India’s nuclear deterrent against China. The missile is likely to support a wide range of warhead configurations, with a 3,500 km range and a total payload weight of 2490 kg. The two-stage solid fuel missile is compact and small enough for easy mobility and flexible deployment on various surface/sub-surface platforms. The last development test of Agni III was conducted in August 2009 before being handed over to the army for user trails.
Agni V Missile with 5000 km
Agni V, believed to be an upgraded version of the Agni III is currently being worked upon by the DRDO. The inter-continental ballistic missile shall have a range of about 5000-6000 km and the first test flight is expected around 2010 end. Agni V would be a three stage solid fueled missile with composite motor casing in the third stage. Agni V will be able to carry multiple warheads and would also display countermeasures against anti-ballistic missile systems.
The Trishul (Trident) is a short range, quick reaction, all weather surface-to-air missile designed to counter a low-level attack. In fact, Trishul was one of the longestrunning DRDO missile development programme. It can also be used as an anti-sea skimmer from a ship against low flying attacking missiles. The missile can engage targets like aircraft and helicopters, flying between 300 m/s and 500 m/s by using its radar commandto- line-of-sight guidance. Powered by a two-stage solid propellant system, with a highly powered HTBP-type propellant similar to the ones used in the Patriot, the Trishul has necessary electronic counter-counter measures against all known aircraft jammers. Trishul, with its quickest reaction time, high frequency operation, high manoeuverability, high lethal capability and multi-roles for three services, is state-of-the-art system providing considerable advantage to the Indian armed forces.
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Agni I Missile MRBM |
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Agni II Missile ICBM |
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Agni I Missile |
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Agni III Missile Ballistic Sysytem |
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Agni III Missile |
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