gptkbp:instance_of
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gptkb:missile
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gptkbp:country_of_origin
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gptkb:India
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gptkbp:deployment
|
various military bases
strategic locations
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gptkbp:design
|
single-stage missile
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gptkbp:developed_by
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gptkb:DRDO
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gptkbp:development
|
gptkb:1983
1983 to 1994
DRDO scientists
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gptkbp:development_cost
|
estimated at $1 billion
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gptkbp:diameter
|
1.0 m
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gptkbp:engine_type
|
liquid fuel
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gptkbp:fighting_style
|
not used in combat yet
|
gptkbp:first_flight
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gptkb:1988
multiple successful tests
multiple test ranges in India
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gptkbp:guidance_system
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gptkb:navigation_system
inertial guidance
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gptkbp:has_programs
|
gptkb:Agni_missile_series
|
https://www.w3.org/2000/01/rdf-schema#label
|
Prithvi Missile
|
gptkbp:involved_technology
|
not applicable
|
gptkbp:launch_platform
|
mobile launcher
mobile command centers
|
gptkbp:launch_site
|
multiple locations in India
|
gptkbp:launch_vehicle
|
mobile launcher vehicle
|
gptkbp:launched
|
road mobile
|
gptkbp:length
|
8.56 m
|
gptkbp:max_speed
|
Mach 5
|
gptkbp:max_takeoff_weight
|
4,600 kg
|
gptkbp:military_branch
|
gptkb:Indian_Armed_Forces
|
gptkbp:notable_mission
|
defense and deterrence
|
gptkbp:operational_range
|
250 km
|
gptkbp:operational_status
|
active
|
gptkbp:operational_use
|
gptkb:1994
|
gptkbp:origin
|
gptkb:India
|
gptkbp:propulsion
|
UDMH and nitrogen tetroxide
|
gptkbp:range
|
150 to 350 km
up to 350 km
|
gptkbp:sales
|
not available for export
|
gptkbp:service_entry
|
gptkb:1994
|
gptkbp:status
|
in service
|
gptkbp:stealth_features
|
limited radar cross-section
|
gptkbp:strategic_importance
|
regional deterrence
tactical nuclear deterrence
|
gptkbp:successor
|
gptkb:Prithvi_II
|
gptkbp:testing_agency
|
gptkb:DRDO
|
gptkbp:type
|
surface-to-surface missile
|
gptkbp:upgrades
|
planned enhancements
|
gptkbp:used_by
|
gptkb:Indian_Armed_Forces
|
gptkbp:user
|
gptkb:Indian_Air_Force
gptkb:Indian_Navy
gptkb:Indian_Army
|
gptkbp:warhead_type
|
nuclear or conventional
|
gptkbp:weight
|
4,600 kg
|
gptkbp:bfsParent
|
gptkb:A._P._J._Abdul_Kalam
|
gptkbp:bfsLayer
|
5
|