| 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 |
