|
gptkbp:instance_of
|
gptkb:missile
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:debut
|
gptkb:1999
|
|
gptkbp:deployment
|
gptkb:1999
gptkb:2004
strategic deterrence
|
|
gptkbp:design
|
gptkb:DRDO
DRDO engineers
|
|
gptkbp:design_features
|
advanced guidance system
multiple warhead capability
|
|
gptkbp:developed_by
|
gptkb:DRDO
|
|
gptkbp:development
|
gptkb:DRDO
gptkb:1995
1990s
1995-1999
|
|
gptkbp:development_cost
|
classified
|
|
gptkbp:diameter
|
1.3 m
|
|
gptkbp:fighting_style
|
long-range strike
nuclear strike
|
|
gptkbp:first_flight
|
gptkb:1999
high
successful
multiple successful tests
|
|
gptkbp:fuel_type
|
gptkb:solid
solid propellant
|
|
gptkbp:global_presence
|
not exported
|
|
gptkbp:guidance_system
|
gptkb:navigation_system
inertial guidance
|
|
gptkbp:has_ability
|
high
|
|
gptkbp:has_programs
|
gptkb:Agni_series
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Agni-II
|
|
gptkbp:integration
|
with Indian defense systems
|
|
gptkbp:involved_technology
|
missile technology
|
|
gptkbp:is_integrated_with
|
with other missile systems
|
|
gptkbp:is_targeted_at
|
300 m
|
|
gptkbp:is_tested_for
|
gptkb:Pokhran
multiple
successful
user trials
|
|
gptkbp:launch_capability
|
mobile and rail
|
|
gptkbp:launch_date
|
gptkb:1999
periodic tests
|
|
gptkbp:launch_platform
|
mobile launcher
|
|
gptkbp:launch_site
|
test range
test range in India
|
|
gptkbp:launch_vehicle
|
mobile launcher
mobile launcher system
road mobile launcher
|
|
gptkbp:launched
|
vertical launch
road mobile
|
|
gptkbp:length
|
20 m
|
|
gptkbp:max_speed
|
Mach 3.5
|
|
gptkbp:max_takeoff_weight
|
17,000 kg
|
|
gptkbp:military_branch
|
gptkb:Indian_Army
|
|
gptkbp:military_doctrine
|
deterrence strategy
|
|
gptkbp:military_strategy
|
second strike capability
|
|
gptkbp:military_technology
|
strategic deterrence
nuclear deterrence
|
|
gptkbp:military_type
|
gptkb:missile
|
|
gptkbp:notable_mission
|
deterrent capability
|
|
gptkbp:number_of_stages
|
two
|
|
gptkbp:operational_deployment_year
|
gptkb:2004
|
|
gptkbp:operational_range
|
2000 km
1500-2000 km
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operational_use
|
strategic missions
|
|
gptkbp:origin
|
gptkb:India
|
|
gptkbp:part_of
|
gptkb:Agni_series
|
|
gptkbp:payload_capacity
|
1000 kg
|
|
gptkbp:project
|
operational testing
production phase
|
|
gptkbp:propulsion
|
solid fuel
|
|
gptkbp:range
|
2000 km
test range in India
|
|
gptkbp:reliability
|
high
|
|
gptkbp:series
|
multiple tests conducted
|
|
gptkbp:significance
|
strategic missile program
|
|
gptkbp:speed
|
Mach 3
|
|
gptkbp:status
|
in service
|
|
gptkbp:strategic_asset
|
gptkb:Indian_military
|
|
gptkbp:strategic_goals
|
deterrence against adversaries
against regional threats
|
|
gptkbp:strategic_importance
|
regional security
nuclear deterrence
deterrence
|
|
gptkbp:successor
|
gptkb:Agni-III
|
|
gptkbp:technology
|
indigenous
|
|
gptkbp:test_range_location
|
Pokhran test range
|
|
gptkbp:type
|
gptkb:missile
intermediate-range ballistic missile
|
|
gptkbp:user
|
gptkb:Indian_Armed_Forces
|
|
gptkbp:warhead_type
|
1000 kg
nuclear
nuclear or conventional
|
|
gptkbp:weight
|
17 tons
|