|
gptkbp:instanceOf
|
gptkb:marine
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
2.11 m
|
|
gptkbp:enteredService
|
1990
|
|
gptkbp:guidanceSystem
|
GPS update
astro-inertial guidance
|
|
gptkbp:length
|
13.42 m
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:maximumSpeed
|
over Mach 24
|
|
gptkbp:NATODesignation
|
gptkb:UGM-133A
|
|
gptkbp:payload
|
up to 8 warheads
|
|
gptkbp:platform
|
gptkb:marine
|
|
gptkbp:propulsion
|
three-stage solid-fuel rocket
|
|
gptkbp:range
|
over 7,800 km
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:Trident_I_C4_missile
|
|
gptkbp:testLaunches
|
over 160 successful tests
|
|
gptkbp:usedBy
|
gptkb:Royal_Navy
gptkb:United_States_Navy
|
|
gptkbp:warheadOptions
|
gptkb:W76
gptkb:W88
|
|
gptkbp:warheadType
|
gptkb:MIRV_(Multiple_Independently_targetable_Reentry_Vehicle)
|
|
gptkbp:weight
|
58,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Lockheed_Martin_Space_Systems
gptkb:LM
gptkb:Lockheed_Martin_Space
gptkb:United_States_Navy_Strategic_Systems_Programs
gptkb:Trident_nuclear_programme
|
|
gptkbp:bfsLayer
|
6
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Trident II D5 missile
|