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Weapons of Mass Destruction (WMD)


R-11FM / SS-1b Scud

Specifications
DIA SS-1b
NATO Scud
Bilateral  
Service R-11FM
OKB/Industry 8K11/8A61FM
Design Bureau OKB-1 NII-88/SKB-385
Approved  
Years of R&D  
Engineering and Testing  
First Flight Test  
IOC  
Deployment began 2/20/1959
Launch system D-1/D-2
Submarine 611 AB Zulu V
Type of Warhead Single, inseparable
Warheads 1
Yield (mt) 0.1/0.5
Payload (t) 975-1000
Total length (m) 10.3
Total length w/o warhead (m)  
Missile Diameter (m) 0.88
Launch Weight (t) 5.4-5.6
Fuel Weight (t)  
Range (km) 150/167
CEP (m) (Russian Sources) 1.5 km on range, 0.75 on azimuth
CEP (m) Western Sources)  
Number of Stages 1
Warheads Deployed  
Booster guidance system Inertial autonomous
Engine Designation  
Propellants Liquid
Fuel Kerosene T-11
Oxidizer 20% UDMH 80% Nitrogen Acid
Burning time (s)  
Verniers Thrust Sea Level/Vacuum (kn)  
Specific Impulse (s)  
Launching Technique Surfaced



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Page last modified: 24-07-2011 04:48:20 ZULU