Agni (missile)

, the missiles in the Agni series are being inducted into service. The family comprises the following: == Agni-I ==

The two-stage Agni technology demonstrator, with a solid-fuel first stage, was first tested at the Interim Test Range in Chandipur in 1989. It was capable of carrying a conventional payload of 1,000 kg (2,200 lb) or a nuclear warhead. This original technology demonstrator evolved into the solid-fuel Agni-1 and Agni-2 missiles. India first developed the two-stage 2000  km range Agni-2, testing it in 1999. It then used the first stage of this system to develop the 700  km range single-stage Agni-1, which was first tested in January 2002 Weighing 12 tonne with a length of 15 metres, Agni-1 has a range of 700–900 km at a speed of 2.5 km/s. On 11 April 2014 the missile was test fired for the first time in a night trial exercise to its full range of 700 km from the Wheeler island off the Odisha coast. The missile randomly picked from the production line was test-fired by the Strategic Forces Command after 11 pm. This test was the first night after 2 previous tests failed due to technical glitches. The missile was test fired from a mobile launcher with logistics support from DRDO at the Integrated Test Range as part of the regular training exercise by the armed forces. With a special weapons load Agni-I can reach 1200 km. As compared to Agni-II, Agni-I is less costly, simple, accurate, and more mobile. == Agni-II ==

|alt=|left Agni-II with a range of 2,000–2,500 km is 20 metres long, has a diameter of one metre, and weighs around 18 tonnes. Agni–II uses solid propellant in both of its two stages. They are claimed to be a part of the "credible deterrence" against China and Pakistan. India stated that its nuclear and missile development programmes are not Pakistan-centric, that the Pakistani threat is only a marginal factor in New Delhi's security calculus, and that Agni is at the heart of deterrence in the larger context of Sino-Indian equation. The 2000 km range nuclear weapon capable missile, already inducted into the country's arsenal, was successfully launched as a training exercise by the Strategic Forces Command on 9 August 2012. India on 7 April 2013 conducted the latest test of its nuclear-capable Agni-II strategic ballistic missile from a missile testing range in Odisha. The test was conducted from Abdul Kalam Island (formerly known as Wheeler Island) in Bhadrak district, by army personnel as part of a training exercise. India successfully conducted the first night trial of nuclear-capable intermediate-range ballistic missile Agni-II from the Abdul Kalam Island of the Odisha coast at 16 Nov 2019. The 20-metre-long, two-stage ballistic missile has a strike range of 2,000 km To 3000 km. It has a launch weight of 17 tonnes and can carry a payload of 1,000 kg. == Agni-III ==

Agni-III is the third in the Agni series of missiles. Agni III uses solid propellant in both stages. the most accurate strategic ballistic missile of its range class in the world. This is of special significance because a highly accurate ballistic missile increases the "kill efficiency" of the weapon; it allows Indian weapons designers to use smaller yield nuclear warheads (200 kiloton thermonuclear or boosted fission) while increasing the lethality of the strike. This permits India to deploy a much larger nuclear force using less fissile/fusion material (plutonium/lithium deuteride) than other nuclear powers. Older ballistic missiles, such as those deployed by earlier nuclear powers required larger yield (1–2 megaton) warheads to achieve the same level of lethality. It has also been reported that with smaller payloads, the Agni-III can hit strategic targets well beyond 3,500  km. == Agni-IV ==

Agni-IV is the fourth in the Agni series of missiles which was earlier known as Agni II prime. Agni-IV was first tested on 15 November 2011 and 19 September 2012 from Wheeler Island off the coast of the eastern state of Orissa for its full range of 4,000 km. The missile lifted off from a road-mobile launcher at 11.48 a.m. and after climbing to an altitude of over 800 km, it re-entered the atmosphere and impacted near the pre-designated target in the Indian Ocean with a remarkable degree of accuracy following a 20-minute flight. Carrying a payload of explosives weighing a tonne, the missile re-entered the atmosphere and withstood temperatures of more than 3,000 °C. With a range of 3,000–4,000 km, Agni-IV bridges the gap between Agni II and Agni III. It was again successfully test-fired on 20 January 2014. Agni IV can take a warhead of 1 tonne. It is designed to increase the kill efficiency along with a higher range performance. Agni IV is equipped with state-of-the-art technologies, that include indigenously developed ring laser gyro and composite rocket motor. It is a two-stage missile powered by solid propellant. Its length is 20 metres and its launch weight is 17 tonnes. == Agni-V ==

Agni-V is a solid fueled intercontinental ballistic missile (ICBM) developed by Defence Research and Development Organisation (DRDO) of India. It will greatly expand India's reach to strike targets more than 7,000 km away. Agni-V was first test fired on 19 April 2012 at 08:07 am IST from Abdul Kalam Island off the coast of Orissa, the test was successful. In January 2015, the canisterized version was successfully tested from Wheeler Island. == Agni-P ==

It is a medium-range ballistic missile under development that incorporates technological advances from Agni-IV and Agni-V projects. Although it looks similar to Agni-III the weight is reduced by half. Agni-P will replace the older generation missile such as Prithvi, Agni-I and Agni-II. == Agni-VI ==

Agni-VI is an intercontinental ballistic missile reported to be in the early stages of development by India and is being developed by the Defence Research and Development Organisation. It is to be the latest and most advanced version of the Agni missile programme. It will be capable of being launched from submarines as well as from land, and will have a strike range of 8,000–10,000 km with MIRVed warheads. == Further developments ==

In May 2008 Indian scientists announced they had developed and patented a path-breaking technology that increases the range of missiles and satellite launch vehicles by at least 40%. The enhanced range is made possible by adding a special-purpose coating of chromium-based material to a rocket's blunt nose cone. The material acts as a reactive-ablative coating that forms a thin low-density gaseous layer at the tip of the rocket as it approaches hypersonic speeds; this super-heated gas layer reduces drag by 47% (at mach 7–8), thereby allowing range enhancements at least 40%. It has been announced that this technology will be incorporated in future Agni deployments after having undergone ranging and calibration tests. == Specifications ==