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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