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gptkbp:instanceOf
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gptkb:marine
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|
gptkbp:accuracy
|
less than 90 m CEP
|
|
gptkbp:alsoKnownAs
|
gptkb:Trident_D5
|
|
gptkbp:awardedContract
|
1983
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|
gptkbp:countryOfOrigin
|
gptkb:United_States
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|
gptkbp:deployment
|
Strategic nuclear deterrent
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|
gptkbp:diameter
|
2.11 m
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|
gptkbp:enteredService
|
1990
|
|
gptkbp:firstFlight
|
1987
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gptkbp:guidanceSystem
|
Inertial guidance
Star sighting
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Trident II missile
|
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gptkbp:length
|
13.42 m
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:NATODesignation
|
gptkb:UGM-133A
|
|
gptkbp:payload
|
Up to 14 W88 or W76 nuclear warheads
|
|
gptkbp:platform
|
gptkb:marine
|
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gptkbp:predecessor
|
gptkb:Trident_I_missile
|
|
gptkbp:propulsion
|
Three-stage solid-fuel rocket
|
|
gptkbp:range
|
over 7,400 km
|
|
gptkbp:status
|
In service
|
|
gptkbp:testLaunches
|
over 170 successful
|
|
gptkbp:usedBy
|
gptkb:Royal_Navy
gptkb:United_States_Navy
|
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gptkbp:warheadType
|
gptkb:Multiple_independently_targetable_reentry_vehicle_(MIRV)
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|
gptkbp:weight
|
58,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Trident_II_Guidance_System
|
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gptkbp:bfsLayer
|
6
|