R-11 / SS-1B SCUD-A
R-300 9K72 Elbrus / SS-1C SCUD-B
| Specifications | ||||
|---|---|---|---|---|
| DIA | SS-1b | SS-1c | SS-1d | SS-1e |
| NATO | Scud-A | Scud-B | Scud-C | Scud-D |
| Bilateral | ||||
| Service | R-11 / R-175 | R-300 | ||
| OKB/Industry | 8K14 | |||
| Design Bureau | Makeyev OKB | Makeyev OKB | Makeyev OKB | Makeyev OKB |
| Approved | ... | ... | ... | ... |
| Years of R&D | ... | ... | ... | ... |
| Engineering and Testing | ... | ... | ... | ... |
| First Flight Test | ... | ... | ... | ... |
| IOC | ... | ... | ... | ... |
| Deployment Date | 1957 | 1965 | 1965 | 1980s |
| Withdrawn | 1978 | |||
| Type of Warhead | HE, CHEM (thickened VX) | |||
| Warheads | 1 | 1 | 1 | 1 |
| Yield | ... | 5-80 kiloton | ... | ... |
| Payload (t) | 770-950 kg | |||
| Total length (m) | 10.25 m | 11.25 m | 11.25 m | 11.25 m |
| Total length w/o warhead (m) | ||||
| Missile Diameter (m) | 0.88 m | 0.88 m | 0.88 m | 0.88 m |
| Launch Weight (t) | 6,300 kg | |||
| Fuel Weight (t) | ||||
| Range(km) | 130 km | 300 km | 575-600km | 700 km |
| CEP (m) (Russian Sources) | ||||
| CEP (m) (Western Sources) | 4,000 m | 900 m | 900 m | 50 m |
| Reaction time | 60 min | |||
| Engine Designation | ... | ... | ... | ... |
| Design Bureau | ... | ... | ... | ... |
| Engine Configuration | One engine | One engine | One engine | One engine |
| Propellants | Liquid Storable | Liquid Storable | Liquid Storable | Liquid Storable |
| Fuel | Kerosene | UDMH | UDMH | UDMH |
| Oxidizer | nitric acid | RFNA (Russian SG-02 Tonka 250) | RFNA (Russian SG-02 Tonka 250) | RFNA (Russian SG-02 Tonka 250) |
| Main Engines Burning time (sec.) | ... | ... | ... | ... |
| Main engines Thrust Sea Level/Vacuum (Tonnes) | ... | ... | ... | ... |
| Main Engines Specific Impulse Sea Level/Vacuum (sec.) | ... | ... | ... | ... |
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