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{{more citations needed|date= March 2016}}
{{Use British English|date=March 2013}}
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*# Medium Range Surface to Air Missile (SAM) ‘Akash’
*# Short Range Surface to Air Missile (SAM) ‘Trishul’
*# Anti-tank Guided Missile (ATGM) ‘Nag’
The [[Agni (missile)|Agni missile]] was initially conceived in the IGMDP as a technology demonstrator project in the form of a re-entry vehicle, and was later upgraded to a ballistic missile with different ranges.<ref name="brahmos-site-igmdp" /> As part of this program, the Interim Test Range at Balasore in Odisha was also developed for missile testing.<ref name="fl-missile-shield">{{cite news
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{{Main|Pakistani missile research and development program|l1=Hatf Program}}
== Prithvi ==
{{main|Prithvi missile}}
The '''Prithvi missile''' (from [[Sanskrit language|Sanskrit]] पृथ्वी ''[[prithvi|{{IAST|pṛthvī}}]]'' "Earth") is a family of tactical [[Surface-to-surface missile|surface-to-surface]] short-range [[ballistic missile]]s (SRBM) and is India's first indigenously developed ballistic missile. Development of the Prithvi began in 1983, and it was first test-fired on 25 February 1988 from Sriharikota, SHAR Centre, Pottisreeramulu Nellore district, Andhra Pradesh. It has a range of up to 150 to 300 km. The land variant is called '''Prithvi''' while the naval operational variant of Prithvi I and Prithvi III class missiles are code named '''Dhanush''' (meaning
The Prithvi is said to have its propulsion technology derived from the Soviet [[SA-2]] surface-to-air missile.<ref>{{cite web|author=John Pike |url=http://www.globalsecurity.org/wmd/world/india/prithvi.htm |title=Prithvi – India Missile Special Weapons Delivery Systems |publisher=GlobalSecurity.org |access-date=2010-10-08}}</ref> Variants make use of either liquid or both liquid and solid fuels. Developed as a battlefield missile, it could carry a nuclear warhead in its role as a tactical [[nuclear weapon]].
{| class="wikitable"
|-
! Missile !! Type !! Warhead !! Payload (kg) !! Range (km) !! Dimension (m) !! Fuel/
|-
| Prithvi-I || Tactical || Nuclear, HE, submunitions, FAE, chemical || 1,000 || 150 || 8.55X1.1 || Single stage liquid || 4,400 || 1988 || 30–50
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The initial project framework of the IGMDP envisioned the Prithvi missile as a short-range ballistic missile with variants for the Indian Army, Indian Air Force and the Indian Navy.<ref>[http://cns.miis.edu/research/india/indiach2.htm Centre for Non Proliferation Studies Archive] {{webarchive|url=http://webarchive.loc.gov/all/20011202044243/http://cns.miis.edu/research/india/indiach2.htm |date=2 December 2001 }} ''accessed'' 18 October 2006.</ref> Over the years the ''Prithvi'' missile specifications have undergone a number of changes. The Prithvi I class of missiles were inducted into the Indian Army in 1994, and it is reported that Prithvi I missiles are being withdrawn from service, being replaced with Prahar missiles.<ref>{{cite web|url=http://defense-update.com/20130701_prahar_to_replace_privthi.html |title=After 17 years in service, the Prithvi I missile will give way to smaller and better Prahar |date=July 2013 |publisher=defense-update.com |access-date=2013-07-01}}</ref> Prithvi II missiles were inducted in 1996. ''Prithvi III'' class has a longer-range of 350 km, and was successfully test fired in 2004.<ref name=janes-dhanush>{{cite web|url=http://www.janes.com/articles/Janes-Naval-Weapon-Systems/Dhanush-Sagarika-Project-K-15-India.html |title=Dhanush/Sagarika (Project K-15) (India) – Jane's Naval Weapon Systems |publisher=Janes.com |access-date=2012-12-24}}</ref>
== Agni
A technology demonstrator for re-entry technology called Agni was added to IGMDP as Prithvi was unable to be converted to a longer ranged missile. The first flight of Agni with re-entry technology took place in 1989.<ref name="frontline-13feb09">{{cite magazine|author=T. S. Subramanian|date=31 January – 13 February 2009|title=Missile shield|url=http://www.frontline.in/static/html/fl2603/stories/20090213260309700.htm|magazine=Frontline|volume=26|issue=3|publisher=Kasturi|issn=0970-1710}}</ref> The re-entry system used resins and carbon fibres in its construction and was able to withstand a temperature of up to 3000 °C.<ref name="frontline-13feb09"/><ref>{{cite magazine|author=T. S. Subramanian|date=21 August 2015|title=Technologist to the core|url=http://www.frontline.in/other/obituary/technologist-to-the-core/article7499055.ece|magazine=Frontline|publisher=Kasturi|issn=0970-1710}}</ref> The technologies developed in this project were eventually used in the [[Agni (missile)|Agni series]] of missiles.<ref>{{cite web|author1=PIB Delhi|title=Missile Development Programme|url=http://pib.nic.in/PressReleseDetail.aspx?PRID=85986|date=13 August 2012}}</ref>
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== Akash ==
{{main|Akash missile}}
[[File:Akash SAM.jpg|thumb|200px|An Akash missile being test fired from the Integrated Test Range (ITR), Chandipur, Orissa. The launch platform is a BMP-2 vehicle.]]
'''Akash''' (Sanskrit: आकाश meaning ''Sky'') is a medium-range surface-to-air missile developed as part of India's Integrated Guided Missile Development Programme to achieve self-sufficiency in the area of surface-to-air missiles. It is the most expensive missile project ever undertaken by the Union government in the 20th century. Development costs skyrocketed to almost {{USD}}120 million, which is far more than other similar systems.<ref name=trishul_shut>[http://www.rediff.com/news/2008/feb/27trishul.htm "India Shuts Down Trishul Missile Project" ] ''[[Rediff.com]]'' 27 February 2008</ref>
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Separate versions for the Army and the Air Force are being developed. For the Army, the missiles will be carried by specialist carrier vehicles (NAMICA-Nag Missile Carrier) equipped with a [[thermographic camera]] for target acquisition. NAMICA is a modified [[BMP-2]] [[infantry fighting vehicle]] licence produced as "Sarath" in India. The carriers are capable of carrying four ready-to-fire missiles in the observation/launch platform which can be elevated with more missiles available for reload within the carrier. For the Air Force, a nose-mounted thermal imaging system has been developed for guiding the missile's trajectory "Helina". The missile has a completely [[fiberglass]] structure and weighs around 42 kg.
Nag was test fired for the 45th time on 19 March 2005 from the Test Range at [[Ahmednagar]] ([[Maharashtra]]), signalling the completion of the developmental phase. It will now enter the production phase, subject to user trials and acceptance by the [[Indian Army]].
Further versions of the missile may make use of an all-weather [[Extremely high frequency|Milli-metre Wave]] (mmW) seeker as an additional option. This seeker has reportedly been developed and efforts are on to integrate it into the missile.
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