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UR-200

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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.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)
Designed
1962
Designer
OKB-52
Diameter
3 m (9.8 ft)
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)
Flight ceiling
185 km (115 mi) apogee

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UR-200

Nodes29
Edges28
Triples42
Avg. degree1.93
Density0.068966
Components1

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UR-200

Top relations

related to FOBS · 10
UR-200 → Earth, FOBS, Fractional Orbital Bombardment System, Nikita Khrushchev, October, R-36, Soviet, The, The FOBS, The UR-200
related to Description · 8
UR-200 → ICBM, It, Nitrogen, R-16, Soviet, The UR-200, UDMH, Unusually
related to Related developments · 5
UR-200 → Mikhail YangelUniversal RocketUR-100, R-9 Desna, Sergei KorolevR-16, UR-100, UR-500
related to history · 3
UR-200 → R-36, The, The UR-200
.mw-parser-output .tooltip-dotted{border-bottom:1px dotted;cursor:help}Maximum speed · 1
UR-200 → Mach 20 (24,500 km/h; 15,200 mph; 6.81 km/s)
Designed · 1
UR-200 → 1962
Designer · 1
UR-200 → OKB-52
Diameter · 1
UR-200 → 3 m (9.8 ft)
Engine · 1
UR-200 → 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)
Flight ceiling · 1
UR-200 → 185 km (115 mi) apogee

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Important terminology

missile soviet union first okb-52 fobs icbm km intercontinental ballistic flight 20 operational udmh orbital clarification needed october 1964 r-16

Entity relationships Subject–Predicate–Object triples

SubjectPredicateObjectConfidenceSrc
UR-200.mw-parser-output .tooltip-dotted{border-bottom:1px dotted;cursor:help}Maximum speedMach 20 (24,500 km/h; 15,200 mph; 6.81 km/s)1.00infobox
UR-200Designed19621.00infobox
UR-200DesignerOKB-521.00infobox
UR-200Diameter3 m (9.8 ft)1.00infobox
UR-200EngineFirst 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)1.00infobox
UR-200Flight ceiling185 km (115 mi) apogee1.00infobox
UR-200Guidance systemInertial1.00infobox
UR-200Height34.65 m (113.7 ft)1.00infobox
UR-200In service1963-19641.00infobox
UR-200Mass135,710 kg (299,190 lb)1.00infobox
UR-200Operational range12,000 kilometres (7,500 mi)1.00infobox
UR-200Place of originSoviet Union1.00infobox
UR-200Propellant.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…1.00infobox
UR-200TypeIntercontinental ballistic missile1.00infobox
UR-200WarheadNuclear warhead1.00infobox
UR-200Wingspan4.2 m (14 ft)1.00infobox

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