|
gptkbp:instanceOf
|
gptkb:marine
|
|
gptkbp:accuracy
|
less than 90 m CEP
|
|
gptkbp:awardedContract
|
1983
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:deployment
|
gptkb:Atlantic_Ocean
gptkb:Pacific_Ocean
|
|
gptkbp:deploymentStart
|
1990
|
|
gptkbp:diameter
|
2.11 m
|
|
gptkbp:enteredService
|
1990
|
|
gptkbp:firstFlight
|
1987
|
|
gptkbp:guidanceSystem
|
Inertial guidance
Star sighting
GPS update
|
|
gptkbp:hasUnit
|
~$30 million (approximate)
|
|
gptkbp:length
|
13.42 m
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:NATODesignation
|
gptkb:UGM-133A
|
|
gptkbp:numberOfStages
|
3
|
|
gptkbp:operatedBy
|
gptkb:Royal_Navy
gptkb:United_States_Navy
|
|
gptkbp:payload
|
Up to 8 W88 or W76 nuclear warheads
|
|
gptkbp:platform
|
gptkb:marine
|
|
gptkbp:primaryMission
|
Strategic nuclear deterrence
|
|
gptkbp:propulsion
|
Solid fuel
|
|
gptkbp:range
|
over 7,400 km
|
|
gptkbp:rocketFamily
|
gptkb:Trident_missile_family
|
|
gptkbp:serviceLifeExtension
|
gptkb:D5LE_program
|
|
gptkbp:status
|
In service
|
|
gptkbp:successor
|
gptkb:Trident_I_(C4)
|
|
gptkbp:testLaunches
|
over 170
|
|
gptkbp:usedBy
|
gptkb:Royal_Navy
gptkb:United_States_Navy
|
|
gptkbp:usedInConflict
|
No
|
|
gptkbp:warheadType
|
gptkb:Multiple_independently_targetable_reentry_vehicle_(MIRV)
|
|
gptkbp:warheadYield
|
W76: 100 kt
W88: 475 kt
|
|
gptkbp:weight
|
58,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Trident_missile_system
gptkb:Trident_ballistic_missiles
gptkb:Trident_missile
|
|
gptkbp:bfsLayer
|
6
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Trident II (D5)
|