gptkbp:instanceOf
|
gptkb:surface-to-air_missile
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
gptkbp:deployment
|
gptkb:McConnell_Air_Force_Base
gptkb:Davis–Monthan_Air_Force_Base
gptkb:Little_Rock_Air_Force_Base
|
gptkbp:diameter
|
3.05 meters
|
gptkbp:displayedAt
|
gptkb:Titan_Missile_Museum
|
gptkbp:engineType
|
LR87 (first stage), LR91 (second stage)
|
gptkbp:enteredService
|
1963
|
gptkbp:guidanceSystem
|
inertial guidance
|
https://www.w3.org/2000/01/rdf-schema#label
|
Titan II Missile
|
gptkbp:length
|
31.4 meters
|
gptkbp:manufacturer
|
gptkb:Glenn_L._Martin_Company
|
gptkbp:notableEvent
|
gptkb:1980_Damascus_accident
|
gptkbp:numberOfStages
|
2
|
gptkbp:platform
|
underground silo
|
gptkbp:predecessor
|
gptkb:Titan_I_Missile
|
gptkbp:propulsion
|
gptkb:Aerozine_50_and_nitrogen_tetroxide
|
gptkbp:range
|
15,000 km
|
gptkbp:retired
|
1987
|
gptkbp:status
|
retired
|
gptkbp:successor
|
gptkb:LGM-118_Peacekeeper
|
gptkbp:usedAs
|
space launch vehicle (Gemini-Titan II, Titan 23G)
|
gptkbp:usedBy
|
gptkb:United_States_Air_Force
|
gptkbp:usedIn
|
gptkb:Project_Gemini
|
gptkbp:warheadType
|
gptkb:W-53_thermonuclear_warhead
|
gptkbp:warheadYield
|
9 megatons
|
gptkbp:website
|
gptkb:Vandenberg_Air_Force_Base
|
gptkbp:weight
|
149,000 kg
|
gptkbp:bfsParent
|
gptkb:Titan_I_Missile
|
gptkbp:bfsLayer
|
7
|