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gptkbp:instanceOf
|
ballistic missile
|
|
gptkbp:construction_cost
|
estimated $100 million
|
|
gptkbp:controls
|
mobile launch system
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:deployedTo
|
strategic deterrence
|
|
gptkbp:developedBy
|
gptkb:DRDO
|
|
gptkbp:diameter
|
1.3 m
|
|
gptkbp:doctrine
|
no first use policy
|
|
gptkbp:firstFlight
|
1999
successful
|
|
gptkbp:firstMatch
|
April 1999
|
|
gptkbp:fuelType
|
solid propellant
|
|
gptkbp:global_presence
|
nuclear capable
|
|
gptkbp:hasArea
|
gptkb:Pokhran
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Agni-II missile
|
|
gptkbp:influence
|
regional power projection
|
|
gptkbp:is_part_of
|
Agni series
|
|
gptkbp:launchDate
|
30 minutes
|
|
gptkbp:launched
|
vertical launch
|
|
gptkbp:launchSite
|
Chandipur
|
|
gptkbp:launchVehicle
|
gptkb:Tatra_truck
|
|
gptkbp:length
|
20 m
|
|
gptkbp:maxTakeoffWeight
|
17,000 kg
|
|
gptkbp:militaryRank
|
deterrence against adversaries
|
|
gptkbp:missileSystem
|
intermediate-range ballistic missile
|
|
gptkbp:navigationEquipment
|
gptkb:GPS
|
|
gptkbp:notableContestants
|
multiple
|
|
gptkbp:operational_status
|
2000
|
|
gptkbp:operationalRange
|
1500-2000 km
|
|
gptkbp:operationalStatus
|
Strategic_Forces_Command
|
|
gptkbp:partnerships
|
gptkb:Israel
gptkb:Russia
gptkb:USA
|
|
gptkbp:primaryUser
|
gptkb:Indian_Armed_Forces
|
|
gptkbp:productionYears
|
1994-1999
|
|
gptkbp:propulsion
|
solid fuel
|
|
gptkbp:provides
|
inertial guidance
within 300 m
|
|
gptkbp:range
|
gptkb:ISRO
2000 km
|
|
gptkbp:relatedPatent
|
gptkb:Agni-V
gptkb:Agni-IV
Agni-I
Agni-III
|
|
gptkbp:releaseFormat
|
mobile launcher
|
|
gptkbp:safety_features
|
limited radar cross-section
|
|
gptkbp:speed
|
gptkb:Mach_3
|
|
gptkbp:status
|
in service
not exported
|
|
gptkbp:strategicGoals
|
second strike capability
|
|
gptkbp:successor
|
Agni-III
|
|
gptkbp:type
|
1000 kg
nuclear or conventional
|
|
gptkbp:weight
|
17 tons
|