Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3.05 m
|
| gptkbp:engineType |
liquid-fueled
|
| gptkbp:enteredService |
1963
|
| gptkbp:firstFlight |
1962
|
| gptkbp:guidanceSystem |
inertial guidance
|
| https://www.w3.org/2000/01/rdf-schema#label |
BGM-20 Titan II
|
| gptkbp:launchWeight |
149,685 kg
|
| gptkbp:length |
31.4 m
|
| gptkbp:manufacturer |
gptkb:Glenn_L._Martin_Company
|
| gptkbp:numberBuilt |
108
|
| gptkbp:numberOfStages |
2
|
| gptkbp:platform |
underground silo
|
| 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:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:usedFor |
nuclear deterrence
space launch vehicle (as Titan II GLV) |
| gptkbp:warheadType |
gptkb:W-53_thermonuclear_warhead
|
| gptkbp:warheadYield |
9 megatons
|
| gptkbp:bfsParent |
gptkb:Cold_War_weapons_of_the_United_States
|
| gptkbp:bfsLayer |
8
|