Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3.05 m
|
| gptkbp:enteredService |
1962
|
| gptkbp:firstFlight |
February 6, 1959
|
| gptkbp:guidanceSystem |
inertial guidance
|
| gptkbp:length |
31.4 m
|
| gptkbp:manufacturer |
gptkb:Glenn_L._Martin_Company
|
| gptkbp:mass |
105,000 kg
|
| gptkbp:nickname |
gptkb:Titan_I
|
| gptkbp:numberBuilt |
108
|
| gptkbp:numberOfStages |
2
|
| gptkbp:platform |
underground silo
|
| gptkbp:predecessor |
gptkb:SM-65_Atlas
|
| gptkbp:propulsion |
liquid oxygen and RP-1
|
| gptkbp:range |
10,200 km
|
| gptkbp:retired |
1965
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:LGM-25C_Titan_II
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:usedIn |
gptkb:Cold_War
|
| gptkbp:warheadType |
gptkb:W38_thermonuclear_warhead
|
| gptkbp:warheadYield |
3.75 megatons of TNT
|
| gptkbp:bfsParent |
gptkb:Strategic_Air_Command
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
HGM-25A Titan I
|