This chart provides information on India’s arsenal of ballistic and cruise missiles. It is updated on a rolling basis to include the dates of the latest tests and other developments as they occur. An asterisk beside a data point indicates that this information did not come from an official source but from a reliable, secondary source.
|Name||Type||Range||Stages/Fuel||Payload Capacity||Last Reported Test||Inducted?||Nuclear Capable?|
|Prithvi-I||Ballistic||150 km||Single/Liquid||800 kg*||May 2007||Y(a)||Y|
|Prithvi-II||Ballistic||350 km||Single/Liquid||500-1,000 kg||June 2019*||Y||Y|
|Dhanush||Ballistic||350 km||Single/Liquid||500 kg||February 2018*||Y*||Y|
|Agni-I||Ballistic||700-900 km||Single/Solid*||1,000 kg*||October 2018*||Y||Y*|
|Agni-II||Ballistic||2,000 km||Two/Solid||1 ton||February 2018*||Y||Y|
|Agni-III||Ballistic||3,500 km||Two/Solid||1.5 tons||April 2017*||Y||Y*|
|Agni-IV||Ballistic||4,000 km||Two/Solid||1,000 kg*||December 2018*||Y*||Y|
|Agni-V||Ballistic||+5,000 km||Three/Solid||1,000 kg*||December 2018||N||Y|
|Prahaar||Ballistic||150 km||Single/Solid||200 kg||September 2018*||N*||N*|
|Pragati||Ballistic*||60-170 km*||Single/Solid*||200 kg||Not Tested||N*||N*|
|K-15 (aka B0-5)||SLBM(b)||750 km*||Two/Solid*||1,000 kg*||August 2018*||Y*||Y*|
|K-4||SLBM*||3,500 km*||Two/Solid*||Unknown||December 2017(c)*||N*||Y*|
|BrahMos||Cruise||290-500 km*||Two/Solid and Liquid(d)||200-300 kg||May 2019||(e)N-I: Y|
|Nirbhay||Cruise||1,000 km||Two/solid and liquid(f)||450 kg*||April 2019||N*||Y*|
|Hypersonic Technology Demonstrator Vehicle (HSTDV)||Cruise(g)||Unknown||One/liquid(h)||Unknown||June 2019(i)||N*||Unknown|
a. The Prithvi-I will reportedly be withdrawn from service and upgraded.
b. Submarine-Launched Ballistic Missile.
c. This test was reportedly not successful.
d. The boost phase is solid-fueled while the cruise phase is powered by a liquid ramjet engine.
e. The BrahMos is deployed on multiple platforms. Each deployment has its own designation. N-I refers to deployments on surface naval vessels. Blocks (B) I-III refer to deployments with the Indian Army. ALCM refers to Air-Launched Cruise Missiles and SLCM refers to Submarine-Launched Cruise Missiles.
f. The boost phase is solid-fueled while the cruise phase is powered by a liquid turbofan engine.
g. The HSTDV is comprised of hypersonic cruise missile technologies.
h. In its first test, the HSTDV was reportedly launched on board an Agni-I, which was to bring it to testing altitude. The vehicle itself is powered by a supersonic combustion ramjet (scramjet) engine fueled by kerosene.
i. This test was reportedly aborted after the Agni-I missile carrying the HSTDV failed to reach testing altitude.