- Agni-II at a GlanceORIGINATED FROM
- IndiaCLASS
- Medium-range ballistic missile (MRBM)POSSESSED BY
- IndiaBASING
- Road/rail-mobileLENGTH
- 20 mDIAMETER
- 1 mLAUNCH WEIGHT
- 17,000 kgPAYLOAD
- Single warhead, 1,000 kgWARHEAD
- Nuclear 150 kt or 200kt, HEPROPULSION
- Two-stage, solid propellantRANGE
- 2,000 – 3,500 kmSTATUS
- OperationalIN SERVICE 2004
.
Agni-II evolutionIn July 1997, India's Defence Research and
Development Organisation (DRDO) began work on the Agni-II. It's an improved
version of the DRDO's Agni technological demonstrator, complete with a
solid-fueled upper stage and new propellant. On April 11, 1999, India conducted
the first Agni-II test. According to reports, the test, which took conducted
from a rail-mobile launcher, was a success.
On January 17, 2001, India performed a second Agni-II flight
test after initiating limited manufacture of the missile. The missile was
brought into service by India's armed forces in 2004, although technical
concerns delayed full operational capability until 2011. The Agni-II has now
been completely incorporated into Indian Army formations under the Strategic
Forces Command. In 2010, a flight test of an extended-range derivative that
became the Agni-IV failed.
Agni-II ConceptThe Agni-II is 20 metres long, 1 metre in
diameter, and weighs 17,000 kilogrammes at launch. It can transport a payload
of up to 1,000 kg across a distance of 2,000 kilometres, most likely a nuclear
weapon with a yield of 150 to 200 kilotons. The two-stage, solid-fueled missile
is guided by an inertial/GPS navigation system and is said to be accurate to 40
m circular error probable (CEP). The missile is outfitted with a finned
manoeuvring reentry vehicle that may be supplied with a terminal guidance
system.
The Agni-II PrimeIndia performed a failed flight test of an
enhanced Agni-II model in 2010. This type is also known as the Agni-IV. The
Agni-IV is made up of a steel-cased, 1.2-meter-diameter first-stage booster and
a carbon-fiber-cased, 1-meter-diameter second-stage booster. Over the original
SLV-3-derived booster, both motors use a simpler thrust vectoring system with
gimbaled thrusters.
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