AGNI 1 & 2 missiles

Agni is an Intermediate Range Ballistic Missile. Agni-I used solid propulsion booster and a liquid 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, which has attempted for the first time in the world. It uses all carbon composite structure for protecting payload during its re-entry phase. The first flight conducted in May 1989, established the re-entry technology and precise guidance to reach the specific target. Agni-I flight trials having proved the long-range technologies, an operational version of agni with solid-solid propulsion system was test fired in April 1999, which is Agni-II with mobile capability.

 

 

 

Agni-2 Missile:

 

The range for Agni-2 is performance, repeated guidance more than 2000 km. The salient features of performance capability and salvo firing the test firings are mobile launch capability, capability. With the completion of above multi-staging, state-of-the-art control and flight trials, the design and development of guidance, re-entry technology and the Trishul Missile is complete. sophisticated on-board packages including Nag Missile: Nag is a third generation anti-advanced communication. Agni-2 has also tank missile with top-attack and fire and been inducted into Services. forget capability