R-1  
Initial Operational Capability (IOC): 1948
Total Production: ?
Also Known As: 8A11 and SS-1 Scunner
Origin: Russia
Corporations: Yuzhnoye
Parent System: R-1
Initial Operational Capability (IOC): 1948
Total Production: ?
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Description: R-1, US/NATO SS-1 Scunner, was the first ballistic missile developed in the Soviet Union. It was influenced by the German V-2. Its propulsion system uses a combination of Alcohol and Liquid Oxygen (LOX) as fuel. R-1 is classified as a short range ballistic missile (SRBM) carrying a 1,000-lb payload at ranges of up to 270 km.

R-1 Specifications

Number of Stages: 1
Dimensions
Diameter: 1,700 millimeter (67 inch)
Length: 17 meter (669 inch)
Wingspan: 3.60 meter
Performance
Ceiling: 77,000 meter
CEP: 8,000 meter
Max Range: 270 kilometer (146 nautical mile)
Speed
Top Speed: 1,465 mps (5,275 kph)
Weight
Thrust: 69,000 pound (31,298 kilogram)
Warhead: 483 kilogram (1,065 pound)
Weight: 12,800 kilogram (28,219 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

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