|
gptkbp:instanceOf
|
gptkb:missile_program
|
|
gptkbp:country
|
gptkb:United_Kingdom
gptkb:United_States
|
|
gptkbp:developedBy
|
gptkb:Lockheed_Martin
|
|
gptkbp:enteredService
|
1981
1990
|
|
gptkbp:firstFlight
|
1979
|
|
gptkbp:guidanceSystem
|
inertial guidance
stellar navigation
|
|
gptkbp:mainContractor
|
gptkb:Lockheed_Martin_Space_Systems
|
|
gptkbp:maximumSpeed
|
over 24,000 km/h
|
|
gptkbp:missionType
|
gptkb:marine
|
|
gptkbp:numberOfStages
|
3
|
|
gptkbp:payload
|
multiple independently targetable reentry vehicles
|
|
gptkbp:platform
|
gptkb:marine
|
|
gptkbp:propulsion
|
solid fuel
|
|
gptkbp:purpose
|
nuclear deterrence
|
|
gptkbp:range
|
over 7,000 km
|
|
gptkbp:replacedBy
|
gptkb:Polaris_missile
gptkb:Poseidon_missile
|
|
gptkbp:rocketFamily
|
gptkb:Trident_II_(D5)
gptkb:Trident_I_(C4)
|
|
gptkbp:status
|
active
|
|
gptkbp:treaty
|
gptkb:START_Treaty
gptkb:New_START_Treaty
|
|
gptkbp:usedBy
|
gptkb:Royal_Navy
gptkb:United_States_Navy
|
|
gptkbp:warheadType
|
gptkb:surface-to-air_missile
thermonuclear
|
|
gptkbp:bfsParent
|
gptkb:United_States_Navy_Strategic_Systems_Programs
|
|
gptkbp:bfsLayer
|
6
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Trident missile program
|