|
gptkbp:instanceOf
|
gptkb:marine
|
|
gptkbp:accuracy
|
90 m CEP
|
|
gptkbp:alliedProgram
|
gptkb:Trident_missile_program
|
|
gptkbp:awardedContract
|
1983
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:deployment
|
Strategic nuclear deterrence
|
|
gptkbp:diameter
|
2.11 m
|
|
gptkbp:enteredService
|
1990
|
|
gptkbp:firstFlight
|
1987
|
|
gptkbp:guidanceSystem
|
gptkb:GPS
Inertial guidance
Star sighting
|
|
gptkbp:length
|
13.42 m
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:nickname
|
gptkb:Trident_D5
|
|
gptkbp:numberOfStages
|
3
|
|
gptkbp:payload
|
Up to 8 MIRVs
|
|
gptkbp:platform
|
gptkb:marine
|
|
gptkbp:predecessor
|
gptkb:UGM-96_Trident_I
|
|
gptkbp:propulsion
|
Solid fuel
|
|
gptkbp:range
|
over 7,800 km
|
|
gptkbp:status
|
In service
|
|
gptkbp:testLaunches
|
over 170
|
|
gptkbp:usedBy
|
gptkb:Royal_Navy
gptkb:United_States_Navy
|
|
gptkbp:warheadType
|
gptkb:W76
gptkb:W88
Multiple independently targetable reentry vehicles (MIRVs)
|
|
gptkbp:weight
|
58,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Trident_II_Guidance_System
|
|
gptkbp:bfsLayer
|
6
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
UGM-133A Trident II
|