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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