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gptkbp:instance_of
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gptkb:missile
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gptkbp:block_variants
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gptkb:Block_IB
gptkb:Block_IIA
gptkb:Block_IIB
Block IA
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gptkbp:collaboration
|
with Japan
with Australia
with NATO
|
|
gptkbp:combat_history
|
none reported
|
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gptkbp:contract
|
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
|
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gptkbp:country
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gptkb:Japan
gptkb:South_Korea
NATO members
|
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gptkbp:developed_by
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gptkb:Raytheon
|
|
gptkbp:development
|
gptkb:1996
|
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gptkbp:development_cost
|
estimated at $3 billion
|
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gptkbp:diameter
|
0.34 m
|
|
gptkbp:engagement_altitude
|
up to 150 km
|
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gptkbp:first_introduced
|
gptkb:2005
|
|
gptkbp:guidance_system
|
active radar homing
inertial guidance with midcourse updates
|
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gptkbp:has_programs
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gptkb:combat_system
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|
https://www.w3.org/2000/01/rdf-schema#label
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SM-3 missile
|
|
gptkbp:integrates_with
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gptkb:Aegis_radar_system
|
|
gptkbp:interception_method
|
hit-to-kill
|
|
gptkbp:is_tested_for
|
gptkb:Pacific_Missile_Range_Facility
multiple successful tests
|
|
gptkbp:key_feature
|
advanced sensor technology
multi-target engagement capability
sea-based deployment
interoperability with allied systems
capability to intercept in midcourse phase
|
|
gptkbp:launch_platform
|
Aegis-equipped ships
Vertical Launch System (VLS)
|
|
gptkbp:length
|
6.55 m
|
|
gptkbp:max_takeoff_weight
|
about 1,500 kg
|
|
gptkbp:notable_work
|
intercepting ballistic missiles
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:operational_use
|
defense against short to intermediate-range ballistic missiles
|
|
gptkbp:part_of
|
gptkb:Aegis_Ballistic_Missile_Defense
|
|
gptkbp:propulsion
|
solid rocket motor
|
|
gptkbp:range
|
gptkb:Pacific_Ocean
up to 2,500 km
|
|
gptkbp:speed
|
approximately Mach 10
|
|
gptkbp:successor
|
gptkb:SM-6_missile
|
|
gptkbp:system
|
theater missile defense
|
|
gptkbp:type
|
anti-ballistic missile
|
|
gptkbp:upgrades
|
planned enhancements for Block IIB
|
|
gptkbp:used_by
|
gptkb:United_States_Navy
|
|
gptkbp:warhead_type
|
kinetic kill vehicle
|
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gptkbp:bfsParent
|
gptkb:SM-6_missile
|
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gptkbp:bfsLayer
|
6
|