|
gptkbp:instanceOf
|
gptkb:surface-to-air_missile
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:deployment
|
gptkb:Strategic_Air_Command
underground silo
|
|
gptkbp:diameter
|
3.05 m
|
|
gptkbp:engineType
|
LR87-AJ-3 (first stage), LR91-AJ-3 (second stage)
|
|
gptkbp:enteredService
|
1962
|
|
gptkbp:firstFlight
|
1959
|
|
gptkbp:guidanceSystem
|
inertial guidance
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Titan I Missile
|
|
gptkbp:lastFlight
|
1965
|
|
gptkbp:launchWeight
|
105,000 kg
|
|
gptkbp:length
|
31.4 m
|
|
gptkbp:manufacturer
|
gptkb:Glenn_L._Martin_Company
|
|
gptkbp:maximumSpeed
|
24,000 km/h
|
|
gptkbp:nickname
|
gptkb:SM-68
|
|
gptkbp:numberOfStages
|
2
|
|
gptkbp:operationalSites
|
18
|
|
gptkbp:platform
|
silo-based
|
|
gptkbp:propulsion
|
liquid oxygen and RP-1
|
|
gptkbp:range
|
10,200 km
|
|
gptkbp:retired
|
1965
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Titan_II_Missile
|
|
gptkbp:testLaunches
|
70
|
|
gptkbp:usedBy
|
gptkb:United_States_Air_Force
|
|
gptkbp:usedIn
|
gptkb:Cold_War
|
|
gptkbp:warheadType
|
gptkb:W38_thermonuclear_warhead
|
|
gptkbp:warheadYield
|
3.75 megatons
|
|
gptkbp:bfsParent
|
gptkb:Cordele,_Georgia,_United_States
|
|
gptkbp:bfsLayer
|
6
|