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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