|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Agni_missile
|
|
gptkbp:country
|
gptkb:India
|
|
gptkbp:deployment
|
strategic locations in India
|
|
gptkbp:design
|
gptkb:DRDO
|
|
gptkbp:developed_by
|
gptkb:DRDO
|
|
gptkbp:developer
|
gptkb:DRDO
1990s
classified
1990s to 2000s
|
|
gptkbp:diameter
|
1.3 m
|
|
gptkbp:enemy
|
nuclear or conventional
|
|
gptkbp:features
|
advanced guidance system
|
|
gptkbp:fighting_style
|
nuclear deterrence
|
|
gptkbp:first_flight
|
gptkb:1999
successful
|
|
gptkbp:global_presence
|
recognized as a strategic weapon
|
|
gptkbp:guidance_system
|
inertial guidance
|
|
gptkbp:has_programs
|
Agni missile program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Agni II
|
|
gptkbp:is_aimed_at
|
within 100 m
|
|
gptkbp:is_tested_for
|
multiple successful tests
Chandipur
|
|
gptkbp:launch_date
|
gptkb:1999
|
|
gptkbp:launch_site
|
mobile launcher
Integrated Test Range
mobile launch system
|
|
gptkbp:launch_vehicle
|
mobile launch vehicle
|
|
gptkbp:launched
|
road mobile
|
|
gptkbp:length
|
20 m
|
|
gptkbp:manufacturer
|
gptkb:Brah_Mos_Aerospace
|
|
gptkbp:military_branch
|
gptkb:military_officer
|
|
gptkbp:military_technology
|
strategic deterrence
|
|
gptkbp:operational_area
|
2000s
|
|
gptkbp:operational_range
|
2000 km
intermediate range
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:origin
|
gptkb:India
|
|
gptkbp:primary_user
|
gptkb:Indian_Armed_Forces
|
|
gptkbp:propulsion
|
solid fuel
|
|
gptkbp:provides_information_on
|
inertial and terminal guidance
|
|
gptkbp:range
|
2000 km
|
|
gptkbp:role
|
strategic deterrence
|
|
gptkbp:seating_capacity
|
1000 kg
|
|
gptkbp:speed
|
Mach 3
|
|
gptkbp:status
|
in service
|
|
gptkbp:strategic_importance
|
high
regional stability
deterrent against regional threats
against adversaries
|
|
gptkbp:successor
|
gptkb:Agni_III
|
|
gptkbp:type
|
intermediate-range ballistic missile
|
|
gptkbp:weight
|
17 tons
|