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gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Agni_missile
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:debut_year
|
gptkb:2012
|
|
gptkbp:defense
|
nuclear defense
|
|
gptkbp:developed_by
|
gptkb:DRDO
|
|
gptkbp:developer
|
gptkb:2009
gptkb:Defence_Research_and_Development_Organisation
|
|
gptkbp:diameter
|
2 meters
|
|
gptkbp:engine_type
|
solid rocket motor
|
|
gptkbp:features
|
multiple independently targetable reentry vehicles (MIR Vs)
|
|
gptkbp:first_flight
|
gptkb:2012
successful
April 19, 2012
|
|
gptkbp:global_presence
|
strategic weapon
|
|
gptkbp:guidance_system
|
inertial guidance system
|
|
gptkbp:has_ability
|
second strike
|
|
gptkbp:headcount
|
1,500 kg
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Agni V
|
|
gptkbp:is_tested_for
|
gptkb:Odisha
multiple
user trial
|
|
gptkbp:launch_date
|
gptkb:2012
|
|
gptkbp:launch_site
|
gptkb:Wheeler_Island
mobile launcher
|
|
gptkbp:launch_vehicle
|
gptkb:Agni_series
|
|
gptkbp:launched
|
road mobile
|
|
gptkbp:length
|
17 meters
|
|
gptkbp:military_branch
|
gptkb:military_officer
|
|
gptkbp:mission
|
deterrence
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_range
|
5,000 km
|
|
gptkbp:operational_status
|
operational
|
|
gptkbp:origin
|
gptkb:India
|
|
gptkbp:primary_user
|
gptkb:Indian_Armed_Forces
|
|
gptkbp:project
|
operational phase
|
|
gptkbp:propulsion
|
solid fuel
|
|
gptkbp:provides_information_on
|
GPS and inertial navigation
|
|
gptkbp:range
|
5,000-8,000 km
|
|
gptkbp:seating_capacity
|
nuclear or conventional warheads
|
|
gptkbp:speed
|
Mach 24
|
|
gptkbp:status
|
in service
|
|
gptkbp:strategic_importance
|
regional security
nuclear deterrence
long-range strike
|
|
gptkbp:successor
|
Agni VI
|
|
gptkbp:technology
|
indigenous technology
|
|
gptkbp:weight
|
50,000 kg
|