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The UGM-27 Polaris missile was a two-stage solid-fueled nuclear-armed submarine-launched ballistic missile (SLBM). As the United States Navy's first SLBM, it served from 1961 to 1980.
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| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| UGM-27 Polaris | .mw-parser-output .tooltip-dotted{border-bottom:1px dotted;cursor:help}Maximum speed | 8,000 mph (13,000 km/h) | 1.00 | infobox |
| UGM-27 Polaris | Accuracy | CEP 3,000 feet (910 m) | 1.00 | infobox |
| UGM-27 Polaris | Blast yield | 1 x 600 kt or 1.2 mt, 3 × 200 kt | 1.00 | infobox |
| UGM-27 Polaris | Designed | 1956–1960 | 1.00 | infobox |
| UGM-27 Polaris | Diameter | 4 ft 6 in (1,370 mm) | 1.00 | infobox |
| UGM-27 Polaris | Engine | First stage, Aerojet General Solid-fuel rocket Second stage, Hercules rocket | 1.00 | infobox |
| UGM-27 Polaris | Guidance system | Inertial | 1.00 | infobox |
| UGM-27 Polaris | Height | 32 ft 4 in (9.86 m) | 1.00 | infobox |
| UGM-27 Polaris | In service | 1961–1996 | 1.00 | infobox |
| UGM-27 Polaris | Launch platform | Ballistic missile submarines | 1.00 | infobox |
| UGM-27 Polaris | Manufacturer | Lockheed Corporation | 1.00 | infobox |
| UGM-27 Polaris | Mass | 35,700 lb (16,200 kg) | 1.00 | infobox |
| UGM-27 Polaris | Operational range | 2,500 nautical miles (4,600 km) | 1.00 | infobox |
| UGM-27 Polaris | Place of origin | United States | 1.00 | infobox |
| UGM-27 Polaris | Propellant | Solid propellant | 1.00 | infobox |
| UGM-27 Polaris | Steering system | Thrust vectoring | 1.00 | infobox |
| UGM-27 Polaris | Type | Submarine-launched ballistic missile | 1.00 | infobox |
| UGM-27 Polaris | Used by | United States Navy, Royal Navy | 1.00 | infobox |
| UGM-27 Polaris | Variants | A-1, A-2, A-3, Chevaline | 1.00 | infobox |
| UGM-27 Polaris | Warhead | 1 x W47, 3 × W58 thermonuclear weapon | 1.00 | infobox |
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