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The UR-200 was an intercontinental ballistic missile (ICBM) developed by Vladimir Chelomey's OKB-52 in the Soviet Union. It was known during the Cold War by the NATO reporting name SS-10 Scrag and internally by the GRAU index 8K81. The design was authorized by the Decisions of the Central Committee of the CPSU of March 16 and August 1, 1961, and the…
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missile soviet union first okb-52 fobs icbm km intercontinental ballistic flight 20 operational udmh orbital clarification needed october 1964 r-16
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| UR-200 | .mw-parser-output .tooltip-dotted{border-bottom:1px dotted;cursor:help}Maximum speed | Mach 20 (24,500 km/h; 15,200 mph; 6.81 km/s) | 1.00 | infobox |
| UR-200 | Designed | 1962 | 1.00 | infobox |
| UR-200 | Designer | OKB-52 | 1.00 | infobox |
| UR-200 | Diameter | 3 m (9.8 ft) | 1.00 | infobox |
| UR-200 | Engine | First stage, RD-0202 liquid-fuel rocket Second stage, RD-0205 liquid-fuel rocket First stage, 2,236 kN (503,000 lbf) Second stage, 606.4 kN (136,300 lbf) | 1.00 | infobox |
| UR-200 | Flight ceiling | 185 km (115 mi) apogee | 1.00 | infobox |
| UR-200 | Guidance system | Inertial | 1.00 | infobox |
| UR-200 | Height | 34.65 m (113.7 ft) | 1.00 | infobox |
| UR-200 | In service | 1963-1964 | 1.00 | infobox |
| UR-200 | Mass | 135,710 kg (299,190 lb) | 1.00 | infobox |
| UR-200 | Operational range | 12,000 kilometres (7,500 mi) | 1.00 | infobox |
| UR-200 | Place of origin | Soviet Union | 1.00 | infobox |
| UR-200 | Propellant | .mw-parser-output .template-chem2-su{display:inline-block;font-size:80%;line-height:1;vertical-align:-0.35em}.mw-parser-output .template-chem2-su>span{display:block;text-align:l… | 1.00 | infobox |
| UR-200 | Type | Intercontinental ballistic missile | 1.00 | infobox |
| UR-200 | Warhead | Nuclear warhead | 1.00 | infobox |
| UR-200 | Wingspan | 4.2 m (14 ft) | 1.00 | infobox |
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