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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.
The analysis highlights History and Measurement as prominent areas in the source structure around UGM-27 Polaris. 1 topic appears in more than one source area, which can help identify connections that are less obvious in a linear reading.
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The extracted context around UGM-27 Polaris shows recurring relationship patterns in the source. For example, UGM-27 Polaris → 8,000 mph (13,000 km/h) Another extracted example is UGM-27 Polaris → CEP 3,000 feet (910 m). Use these groups to spot repeated connection types before inspecting the individual relationships.
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TTTA extracted 20 structured relationships around UGM-27 Polaris. Examples in this analysis include UGM-27 Polaris → .mw-parser-output .tooltip-dotted{border-bottom:1px dotted;cursor:help}Maximum speed → 8,000 mph (13,000 km/h) and UGM-27 Polaris → Accuracy → CEP 3,000 feet (910 m). The table shows each extracted connection, where it came from and its confidence.
| 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 |
The concept neighborhoods around UGM-27 Polaris bring nearby vocabulary together. In this analysis, examples include Us, Missiles and Program. Use the clusters to find adjacent concepts and terminology that may deserve separate research.
For UGM-27 Polaris, one of the stronger structural bridges in this analysis connects UGM-27 Polaris with History and development. Bridges highlight paths between different parts of the map and can reveal research angles that are easy to miss in a flat list.
TTTA analyzes the structure around UGM-27 Polaris to surface related topics, entities, relationships, concept neighborhoods and bridge connections. Use the map to explore areas such as History & Measurement, including less central topics that may reveal useful research gaps. Automatically extracted connections are research leads rather than rewritten encyclopedia content.
Source: Wikipedia — UGM-27 Polaris · EN edition · Analysis: TopicsToTalkAbout
