dbo:Weapon/diameter
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dbo:Weapon/length
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dbo:Weapon/weight
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dbo:abstract
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- Agni-I (Agnī "Fire") is a medium-range ballistic missile that was developed by DRDO of India in the Integrated Guided Missile Development Program. It is a single-stage missile that was developed after the Kargil War to fill the gap between the 250 km (160-mile) range of the Prithvi-II missile and the 2,500 km (1,600-mile) range of the Agni-II. It was first launched from a road mobile launcher at Integrated Test Range (ITR), Wheeler Island, on 25 January 2002. Less than 75 launchers are deployed. (en)
- Agni I est un missile balistique à courte portée (700 kilomètres) développé par l'Inde qui a été testé pour la première fois en 1994 et est déployé depuis 2007. C'est la première version opérationnelle de la famille de missiles Agni. Il emporte une ogive nucléaire de 40 kilotonnes d'équivalent TNT. (fr)
- Agni-I (IAST: Agnī, yang berarti api; juga dewa api Veda dalam agama Hindu) adalah rudal balistik jarak pendek yang dikembangkan oleh DRDO India dalam Integrated Guided Missile Development Program. Ini adalah rudal satu-tahap yang dikembangkan setelah Perang Kargil untuk mengisi celah antara jarak 250 km (160 mil) dari rudal dan jarak 2.500 km (1.600 mil) dari Agni-II. Rudal ini pertama kali diluncurkan dari peluncur jalan di Integrated Test Range (ITR), Pulau Wheeler, pada 25 Januari 2002. Kurang dari 75 peluncur ditembakkan. (in)
- 아그니 1호는 인도 DRDO가 개발한 중거리 탄도 미사일이다. 1999년 5월 카르길 전쟁 이후에 사거리 250 km인 프리트비 2호와 2,500 km인 와의 갭을 메우기 위해 개발이 시작되었다. 무게 12톤, 탄두중량 1톤의 1단 고체로켓이며, 사거리는 1250 km이다. 2004년 실전배치되었다. GPS 유도를 하여 CEP 25 m로 매우 정밀하다. 단가는 560만~790만 달러로서 대략 80억원 정도 한다. (ko)
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dbo:diameter
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dbo:length
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dbo:origin
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dbo:thumbnail
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dbo:weight
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- 12000000.000000 (xsd:double)
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dbo:wikiPageExternalLink
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dbo:wikiPageID
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dbo:wikiPageLength
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- 14555 (xsd:nonNegativeInteger)
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dbo:wikiPageRevisionID
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dbo:wikiPageWikiLink
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dbp:accuracy
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dbp:caption
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- 0001-07-13 (xsd:gMonthDay)
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dbp:ceiling
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dbp:designer
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dbp:diameter
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dbp:engine
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dbp:filling
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- Conventional high explosive-unitary, penetration, cluster munition, incendiary, thermobaric, strategic nuclear weapon (en)
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dbp:fillingWeight
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dbp:guidance
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- Terminal: Radar scene correlation (en)
- Mid-course: Ring laser gyro inertial navigation system. Optionally augmented by GPS/NavIC satellite guidance (en)
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dbp:imageSize
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dbp:isMissile
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dbp:launchPlatform
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dbp:length
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dbp:manufacturer
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dbp:name
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dbp:number
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dbp:origin
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dbp:propellant
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dbp:service
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dbp:speed
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dbp:type
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- Medium Range Ballistic Missile (en)
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dbp:unitCost
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dbp:usedBy
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dbp:vehicleRange
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dbp:weight
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dbp:wikiPageUsesTemplate
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dcterms:subject
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gold:hypernym
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rdf:type
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rdfs:comment
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- Agni-I (Agnī "Fire") is a medium-range ballistic missile that was developed by DRDO of India in the Integrated Guided Missile Development Program. It is a single-stage missile that was developed after the Kargil War to fill the gap between the 250 km (160-mile) range of the Prithvi-II missile and the 2,500 km (1,600-mile) range of the Agni-II. It was first launched from a road mobile launcher at Integrated Test Range (ITR), Wheeler Island, on 25 January 2002. Less than 75 launchers are deployed. (en)
- Agni I est un missile balistique à courte portée (700 kilomètres) développé par l'Inde qui a été testé pour la première fois en 1994 et est déployé depuis 2007. C'est la première version opérationnelle de la famille de missiles Agni. Il emporte une ogive nucléaire de 40 kilotonnes d'équivalent TNT. (fr)
- Agni-I (IAST: Agnī, yang berarti api; juga dewa api Veda dalam agama Hindu) adalah rudal balistik jarak pendek yang dikembangkan oleh DRDO India dalam Integrated Guided Missile Development Program. Ini adalah rudal satu-tahap yang dikembangkan setelah Perang Kargil untuk mengisi celah antara jarak 250 km (160 mil) dari rudal dan jarak 2.500 km (1.600 mil) dari Agni-II. Rudal ini pertama kali diluncurkan dari peluncur jalan di Integrated Test Range (ITR), Pulau Wheeler, pada 25 Januari 2002. Kurang dari 75 peluncur ditembakkan. (in)
- 아그니 1호는 인도 DRDO가 개발한 중거리 탄도 미사일이다. 1999년 5월 카르길 전쟁 이후에 사거리 250 km인 프리트비 2호와 2,500 km인 와의 갭을 메우기 위해 개발이 시작되었다. 무게 12톤, 탄두중량 1톤의 1단 고체로켓이며, 사거리는 1250 km이다. 2004년 실전배치되었다. GPS 유도를 하여 CEP 25 m로 매우 정밀하다. 단가는 560만~790만 달러로서 대략 80억원 정도 한다. (ko)
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rdfs:label
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- Agni-I (en)
- Agni I (fr)
- Agni-I (in)
- 아그니 1호 (ko)
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