gptkbp:instance_of
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gptkb:missile
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gptkbp:associated_with
|
Indian missile program
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gptkbp:control_system
|
digital control system
|
gptkbp:country
|
gptkb:India
|
gptkbp:deployment
|
gptkb:2003
quick deployment
|
gptkbp:design
|
gptkb:DRDO
|
gptkbp:design_features
|
stealth features
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gptkbp:developed_by
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gptkb:DRDO
|
gptkbp:development
|
gptkb:1980s
|
gptkbp:development_cost
|
estimated $30 million
|
gptkbp:diameter
|
1.1 m
|
gptkbp:engine_type
|
solid fuel
|
gptkbp:exported_to
|
gptkb:none
|
gptkbp:fighting_style
|
limited combat use
|
gptkbp:first_flight
|
gptkb:1996
successful
|
gptkbp:guidance_system
|
inertial guidance
|
gptkbp:has_ability
|
precision strike capability
|
https://www.w3.org/2000/01/rdf-schema#label
|
Prithvi-II
|
gptkbp:integration
|
integrated with Indian Army
|
gptkbp:is_tested_for
|
Chandipur
user trials
multiple test launches
|
gptkbp:launch_platform
|
mobile launcher
mobile launcher system
|
gptkbp:launch_vehicle
|
mobile launcher vehicle
|
gptkbp:launched
|
vertical launch
|
gptkbp:length
|
8.56 m
|
gptkbp:manufacturer
|
gptkb:Bharat_Dynamics_Limited
|
gptkbp:max_takeoff_weight
|
4,600 kg
|
gptkbp:military_branch
|
gptkb:Indian_Army
|
gptkbp:military_technology
|
military applications
|
gptkbp:operational_range
|
250 km
|
gptkbp:operational_status
|
operational
|
gptkbp:operational_theater
|
theater of operations in India
|
gptkbp:part_of
|
gptkb:Prithvi_series
|
gptkbp:payload_capacity
|
1,000 kg
|
gptkbp:project
|
completed
|
gptkbp:provides_guidance_on
|
GPS aided inertial navigation
|
gptkbp:range
|
gptkb:Balasore
150 to 250 km
|
gptkbp:reliability
|
high reliability
|
gptkbp:speed
|
Mach 2.0
|
gptkbp:status
|
in service
|
gptkbp:strategic_importance
|
regional deterrence
tactical strike
|
gptkbp:successor
|
gptkb:Agni_series
Prithvi-III
|
gptkbp:type
|
gptkb:missile
|
gptkbp:user
|
gptkb:Indian_Armed_Forces
|
gptkbp:warhead_type
|
conventional or nuclear
|
gptkbp:weight
|
1,000 kg
|
gptkbp:bfsParent
|
gptkb:Prithvi_missile
|
gptkbp:bfsLayer
|
7
|