|
gptkbp:instanceOf
|
gptkb:surface-to-air_missile
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:deployment
|
gptkb:Arizona
gptkb:Arkansas
gptkb:Kansas
54 silos
|
|
gptkbp:diameter
|
3.05 m
|
|
gptkbp:engineType
|
LR87 (first stage), LR91 (second stage)
|
|
gptkbp:enteredService
|
1963
|
|
gptkbp:firstFlight
|
1962
|
|
gptkbp:guidanceSystem
|
inertial guidance
|
|
gptkbp:launchWeight
|
149,685 kg
|
|
gptkbp:length
|
31.4 m
|
|
gptkbp:manufacturer
|
gptkb:Glenn_L._Martin_Company
|
|
gptkbp:maximumSpeed
|
24,000 km/h
|
|
gptkbp:NATOReportingName
|
SS-9 Scarp (erroneously applied by NATO)
|
|
gptkbp:numberOfStages
|
2
|
|
gptkbp:payload
|
single warhead
|
|
gptkbp:platform
|
underground silo
|
|
gptkbp:predecessor
|
gptkb:Titan_I_ICBM
|
|
gptkbp:propulsion
|
gptkb:Aerozine_50_and_nitrogen_tetroxide
|
|
gptkbp:range
|
15,000 km
|
|
gptkbp:retired
|
1987
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:LGM-30_Minuteman
|
|
gptkbp:usedAs
|
basis for Titan II space launch vehicle
|
|
gptkbp:usedBy
|
gptkb:United_States_Air_Force
|
|
gptkbp:warheadType
|
gptkb:W-53_thermonuclear_warhead
|
|
gptkbp:warheadYield
|
9 megatons
|
|
gptkbp:bfsParent
|
gptkb:Atlas_F_ICBM
gptkb:Titan_23B
gptkb:Titan_23G
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Titan II ICBM
|