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R-14 / SS-5 SKEAN
| Specifications | |||||
|---|---|---|---|---|---|
| DIA | SS-5 | SS-5 | |||
| NATO | Skean | Skean | |||
| Bilateral | R-14 | R-14U | |||
| Service | R-14 | R-14U (Chusovaya) | |||
| OKB/Industry | 8K65 | 8K65U | |||
| Design Bureau | OKB-586 | OKB-586 (Acad. M. K. Yangel) | |||
| Approved | 7/2/1958 | 5/30/1960 | |||
| Years of R&D | 1958 - 1960 | 1960 -1962 | |||
| Engineering and Testing | 1960 -1961 | 1961 -1962 | |||
| First Flight Test | 7/6/1960 | 2/11/62 (1/12/1962) | |||
| IOC | 1962 | 1962 | |||
| Deployment Date | 4/24/1961 | 1/9/1964 | |||
| Type of Warhead | Single | Single | |||
| Warheads | 1 | 1 | |||
| Yield (Mt) | 1.0 or 2.0 -2.3 | 1 x 2.3 | |||
| Payload (t) | 1.300 -1.500 or 2.155 | 1.300 -1.500 or 2.155 | |||
| Total length (m) | 24.3 - 24.4 | 24.3 -24.4 | |||
| Total length w/o Warhead (m) |
21.62 | 21.62 | |||
| Missile Diameter (m) | 2.4 | 2.4 | |||
| Launch Weight (t) | 86.3 - 87 | 86.3 | |||
| Fuel Weight (t) | 79.2 | 79.2 | |||
| Range (km) | 4500 or 3200 -3700 | 4500 -3700 | |||
| CEP (m) (Russian Sources) |
1250 -1900 | 1250 | |||
| CEP (m) (Western Sources) |
900-1900 | 900-1900 | |||
| Basing mode | Ground Based | Ground and Silo Based | |||
| Number of Stages | 1 |
| Booster guidance system | Inertial, autonomous |
| Engine Designation | RD-216m (8D514,M) |
| Configuration | Cluster of two engines |
| Design Bureau | Acad. V. P. Glushko OKB-456 |
| Years R & D | 1958-1960 |
| Propellants | Liquid Storable |
| Fuel | UDMH |
| Oxidizer | AK-27 I = IRFNA =73% HN03 + 27% N204 (NTO) in N02 |
| Burning time (sec.) | 130 -131 |
| Thrust Sea Level/Vacuum (Tonnes) | 151.4991/171.075 -177.9Total thrust |
| Specific Impulse Sea Level/Vacuum (sec.) | 246-248 / 290-291.3 |
| Canister length (m) N/A Canister length w/o front meters N/A Canister diameter (m) N/A |
| Hardness | |
| Launching Technique | Hot launched |
| Deployed boosters | 0 |
| Test Boosters | |
| Warheads Deployed | 0 |
| Deployment Sites | INF Treaty Information |
| Training Launchers | |
| Space Booster Variant | SL-8/C-1 Kosmos, Kosmos-3M |
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