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{{more citations needed|date= March 2016}}
{{Short description|Indian Ministry of Defence programme}}
{{Use British English|date=March 2013}}
{{more citations needed|date= March 2022}}
{{Use dmy dates|date=March 2013}}
{{Use British English|date=March 2022}}
{{Use dmy dates|date=April 2022}}
[[File:Agni-V missile during rehearsal of Republic Day Parade 2013.jpg|thumb|300px|Agni-V missile during rehearsal of Republic Day Parade 2013]]
[[File:Agni-V missile during rehearsal of Republic Day Parade 2013.jpg|thumb|300px|Agni-V missile during rehearsal of Republic Day Parade 2013]]
The '''Integrated Guided Missile Development Programme''' (IGMDP) was an Indian [[Ministry of Defence (India)|Ministry of Defence]] programme for the [[research and development]] of the comprehensive range of [[missile]]s. The programme was managed by the [[Defence Research and Development Organisation]] (DRDO) and [[Ordnance Factories Board]]<ref>{{cite web|url=http://ofb.gov.in/units/index.php?unit=ofi&page=my_2&lang=en |title=Indian Ordnance Factories: Ordnance Factory Itarsi |publisher=Ofb.gov.in |access-date=2012-12-24}}</ref> in partnership with other [[Indian government]] political organisations.<ref name="brahmos-site-igmdp">{{cite web
The '''Integrated Guided Missile Development Programme''' ('''IGMDP''') was an Indian [[Ministry of Defence (India)|Ministry of Defence]] programme for the [[research and development]] of the comprehensive range of [[missile]]s. The programme was managed by the [[Defence Research and Development Organisation]] (DRDO) and [[Ordnance Factories Board]]<ref>{{cite web|url=http://ofb.gov.in/units/index.php?unit=ofi&page=my_2&lang=en |title=Indian Ordnance Factories: Ordnance Factory Itarsi |publisher=Ofb.gov.in |access-date=2012-12-24}}</ref> in partnership with other [[Indian government]] political organisations.<ref name="brahmos-site-igmdp">{{cite web
  |title      = Integrated Guided Missile Development Program
  |title      = Integrated Guided Missile Development Program
  |url        = http://brahmos.com/content.php?id=10&sid=25  
  |url        = http://brahmos.com/content.php?id=10&sid=25
|website    = brahmos.com
  |access-date  = 9 June 2012
  |access-date  = 9 June 2012
  |url-status     = dead
  |url-status   = dead
  |archive-url  = https://web.archive.org/web/20120321081536/http://brahmos.com/content.php?id=10&sid=25
  |archive-url  = https://web.archive.org/web/20120321081536/http://brahmos.com/content.php?id=10&sid=25
  |archive-date = 21 March 2012
  |archive-date = 21 March 2012
|df          = dmy-all
}}</ref> The project started in 1982–83 under the leadership of [[A. P. J. Abdul Kalam|Abdul Kalam]] who oversaw its ending in 2008 after these strategic missiles were successfully developed.
}}</ref> The project started in 1982–83 under the leadership of [[A. P. J. Abdul Kalam|Abdul Kalam]] who oversaw its ending in 2008 after these strategic missiles were successfully developed.


On 8 January 2008, the DRDO formally announced the successful rated guided missile programme was completed with its design objectives achieved since most of the missiles in the programme had been developed and inducted by the [[Indian armed forces]].<ref name="hindu-igmdp-over">{{cite news
On 8 January 2008, the DRDO formally announced the successful rated guided missile programme was completed with its design objectives achieved since most of the missiles in the programme had been developed and inducted by the [[Indian armed forces]].<ref name="hindu-igmdp-over">{{cite news
  | title = India scraps integrated guided missile programme
  | title = India scraps integrated guided missile programme
  | newspaper = The Hindu
  | newspaper = [[The Hindu]]
  | location = Chennai, India
  | location = Chennai, India
  | date = 9 January 2008
  | date = 9 January 2008
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This led to the birth of the Integrated Guided Missile Development Programme with [[Abdul Kalam|Dr. Abdul Kalam]], who had previously been the project director for the [[Satellite Launch Vehicle|SLV-3 programme]] at [[ISRO]], was inducted as the DRDL Director in 1983 to conceive and lead it. While the scientists proposed the development of each missile consecutively, the Defence Minister R. Venkataraman asked them to reconsider and develop all the missiles simultaneously. Thus, four projects, to be pursued concurrently, were born under the IGMDP:
This led to the birth of the Integrated Guided Missile Development Programme with [[Abdul Kalam|Dr. Abdul Kalam]], who had previously been the project director for the [[Satellite Launch Vehicle|SLV-3 programme]] at [[ISRO]], was inducted as the DRDL Director in 1983 to conceive and lead it. While the scientists proposed the development of each missile consecutively, the Defence Minister R. Venkataraman asked them to reconsider and develop all the missiles simultaneously. Thus, four projects, to be pursued concurrently, were born under the IGMDP:
* Short range surface-to-surface missile (code-named [[Prithvi (missile)|Prithvi]])
* Dr. APJ Abdul Kalam started multiple projects simultaneously to develop the following types of Indian Guided Missiles missiles.
* Short range low-level surface-to-air missile (code-named [[Trishul (missile)|Trishul]])
*# Short Range Surface to Surface Missile (SSM) ‘Prithvi’
* Medium range surface-to-air missile (code-named [[Akash (missile)|Akash]]) and
*# Long Range Surface to Surface Missile (SSM) ‘Agni’
* Third-generation anti-tank missile (code-named [[Nag (missile)|Nag]]).
*# Medium Range Surface to Air Missile (SAM) ‘Akash’
*# Short Range Surface to Air Missile (SAM) ‘Trishul’
*# Anti-tank Guided Missile (ATGM) ‘Nag’ ([https://www.itworkss.in/best-indian-guided-missiles-part-1/ Read More] )


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
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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  |archive-url=https://web.archive.org/web/20130207034302/http://www.frontlineonnet.com/fl2603/stories/20090213260309700.htm  
  |archive-url=https://web.archive.org/web/20130207034302/http://www.frontlineonnet.com/fl2603/stories/20090213260309700.htm  
  |archive-date=7 February 2013  
  |archive-date=7 February 2013  
|df=dmy-all
}}</ref>
}}</ref>


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{{main|Prithvi missile}}
{{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&nbsp;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 '''Bow'''). Both variants are used for surface targets.
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&nbsp;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 '''Bow'''). Both variants are used for surface targets.


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]].
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"
{| class="wikitable"
|-
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== Agni Re-entry Technology ==
== Agni Re-entry Technology ==
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&nbsp;°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>
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&nbsp;°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 2022}}</ref>


== Trishul ==
== Trishul ==
{{main|Trishul (missile)}}
{{main|Trishul (missile)}}
'''Trishul''' ([[Sanskrit]]: त्रिशूल, meaning ''[[trident]]'') is the name of a short range [[surface-to-air missile]] developed by India as a part of the Integrated Guided Missile Development Program. It has a range of 12&nbsp;km and is fitted with a 5.5&nbsp;kg [[warhead]]. Designed to be used against low-level (sea skimming) targets at short range, the system has been developed to defend [[naval]] vessels against missiles and also as a short-range surface-to-air missile on land. According to reports, the range of the missile is 12&nbsp;km and is fitted with a 15&nbsp;kg warhead. The weight of the missile is 130&nbsp;kg. The length of the missile is 3.1 m.<ref>{{cite web|url=http://www.india-defence.com/reports-3210 |title=Trishul Surface To Air Missile Not A Failure Says Government |publisher=India-defence.com |date=17 May 2007 |access-date=2010-08-31}}</ref> India officially shut down the project on 27 February 2008.<ref name=trishul_shut/> In 2003, Defence Minister [[George Fernandes]] had indicated that the Trishul missile had been de-linked from user service and would be continued as a technology demonstrator.
'''Trishul''' ([[Sanskrit]]: त्रिशूल, meaning ''[[trident]]'') is the name of a short range [[surface-to-air missile]] developed by India as a part of the Integrated Guided Missile Development Program. It has a range of 12&nbsp;km and is fitted with a 5.5&nbsp;kg [[warhead]]. Designed to be used against low-level (sea skimming) targets at short range, the system has been developed to defend [[naval]] vessels against missiles and also as a short-range surface-to-air missile on land. According to reports, the range of the missile is 12&nbsp;km and is fitted with a 15&nbsp;kg warhead. The weight of the missile is 130&nbsp;kg. The length of the missile is 3.5 m.<ref>{{cite web|url=http://www.india-defence.com/reports-3210 |title=Trishul Surface To Air Missile Not A Failure Says Government |publisher=India-defence.com |date=17 May 2007 |access-date=2010-08-31}}</ref> India officially shut down the project on 27 February 2008.<ref name=trishul_shut/> In 2003, Defence Minister [[George Fernandes]] had indicated that the Trishul missile had been de-linked from user service and would be continued as a technology demonstrator.


== Akash ==
== Akash ==
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The first test flight of Akash missile was conducted in 1990, with development flights up to March 1997.
The first test flight of Akash missile was conducted in 1990, with development flights up to March 1997.


The IAF has initiated the process to induct the [[Akash missile|Akash]] [[surface-to-air missile]]s developed as a part of the Integrated Guided Missile Development Programme. The Multiple target handling capability of Akash weapon system was demonstrated by live firing in a C4I environment during the trials. Two Akash missiles intercepted two fast moving targets in simultaneous engagement mode in 2005 itself. The Akash System's 3-D central acquisition radar (3-D car) group mode performance was then fully established.<ref>{{cite web |url=http://frontierindia.net/iaf-initiates-process-for-inducting-akash-and-trishul-sams/ |title=IAF initiates process for inducting Akash and Trishul SAM's |publisher=Frontierindia.net |date=3 May 2007 |access-date=2010-08-31 |url-status=dead |archive-url=https://web.archive.org/web/20100325051818/http://frontierindia.net/iaf-initiates-process-for-inducting-akash-and-trishul-sams/ |archive-date=25 March 2010 |df=dmy-all }}</ref><ref>{{cite web|url=http://www.india-defence.com/reports-3629 |title=Air Force Impressed With Akash Surface To Air Missiles Performance |publisher=India-defence.com |access-date=2010-08-31}}</ref>
The IAF has initiated the process to induct the [[Akash missile|Akash]] [[surface-to-air missile]]s developed as a part of the Integrated Guided Missile Development Programme. The Multiple target handling capability of Akash weapon system was demonstrated by live firing in a C4I environment during the trials. Two Akash missiles intercepted two fast moving targets in simultaneous engagement mode in 2005 itself. The Akash System's 3-D central acquisition radar (3-D car) group mode performance was then fully established.<ref>{{cite web |url=http://frontierindia.net/iaf-initiates-process-for-inducting-akash-and-trishul-sams/ |title=IAF initiates process for inducting Akash and Trishul SAM's |publisher=Frontierindia.net |date=3 May 2007 |access-date=2010-08-31 |url-status=dead |archive-url=https://web.archive.org/web/20100325051818/http://frontierindia.net/iaf-initiates-process-for-inducting-akash-and-trishul-sams/ |archive-date=25 March 2010 }}</ref><ref>{{cite web|url=http://www.india-defence.com/reports-3629 |title=Air Force Impressed With Akash Surface To Air Missiles Performance |publisher=India-defence.com |access-date=2010-08-31}}</ref>


In December 2007 [[Indian Air Force]] completed user trials for the Akash missile system. The trials, which were spread over ten days, were successful, and the missile hit its target on all five occasions. Before the ten-day trial at Chandipur, the Akash system's ECCM Evaluation tests were carried out at Gwalior Air force base while mobility trials for the system vehicles were carried out at Pokhran. The IAF had evolved the user Trial Directive to verify the Akash's consistency in engaging targets. The following trials were conducted: Against low-flying near-range target, long-range high-altitude target, crossing and approaching target and ripple firing of two missiles from the same launcher against a low-altitude receding target.<ref>[http://www.drdo.com/bnews/jan08/akash_test.htm "DRDO report on Akash Air Defence Weapon System"]''[[DRDO]]''</ref>
In December 2007 [[Indian Air Force]] completed user trials for the Akash missile system. The trials, which were spread over ten days, were successful, and the missile hit its target on all five occasions. Before the ten-day trial at Chandipur, the Akash system's ECCM Evaluation tests were carried out at Gwalior Air force base while mobility trials for the system vehicles were carried out at Pokhran. The IAF had evolved the user Trial Directive to verify the Akash's consistency in engaging targets. The following trials were conducted: Against low-flying near-range target, long-range high-altitude target, crossing and approaching target and ripple firing of two missiles from the same launcher against a low-altitude receding target.<ref>[http://www.drdo.com/bnews/jan08/akash_test.htm "DRDO report on Akash Air Defence Weapon System"]''[[DRDO]]''</ref>
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==See also==
==See also==
{{Portal|India}}
{{Portal|India|Rocketry}}
* [[Rajendra Radar]]
* [[Rajendra Radar]]
* [[SA-6|SA-6 Gainful]]
* [[SA-6|SA-6 Gainful]]
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== External links ==
== External links ==
* [http://missilethreat.csis.org/india/ CSIS Missile Threat - India]
* [http://missilethreat.csis.org/india/ CSIS Missile Threat India]
* [https://web.archive.org/web/20061105011002/http://www.bharat-rakshak.com/MISSILES/Akash.html Bharat Rakshak's page of Akash]
* [https://web.archive.org/web/20061105011002/http://www.bharat-rakshak.com/MISSILES/Akash.html Bharat Rakshak's page of Akash]
* [https://web.archive.org/web/20061105010952/http://www.bharat-rakshak.com/MISSILES/Trishul.html Bharat Rakshak's page on Trishul]
* [https://web.archive.org/web/20061105010952/http://www.bharat-rakshak.com/MISSILES/Trishul.html Bharat Rakshak's page on Trishul]
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== References ==
== References ==
{{Reflist|30em}}
{{Reflist}}


{{Indian missiles}}
{{Indian missiles}}