R-31 / RSM-45 SS-N-17 SNIPE
| Specifications | ||
|---|---|---|
| DIA | SS-N-17 | |
| NATO | Snipe | |
| Bilateral | RSM-45 | |
| Service | R-31 | |
| OKB/Industry | 3M17 | |
| Design Bureau | KB Arsenal | |
| Approved | ||
| Years of R&D | ||
| Engineering and Testing | ||
| First Flight Test | 1973 | |
| IOC | ||
| Deployment Date | September 1980 | |
| Launch system | D-11 with 12 missiles | |
| Submarine | Yankee II | |
| Type of Warhead | Single | |
| Warheads | 1 | |
| Yield (mt) | 0.5 | |
| Payload (t) | 0.45 | |
| Total length (m) | 11 | |
| Total length w/o warhead (m) | 10.6 | |
| Missile Diameter (m) | 1.54 | |
| Diameter of Stabilizers (m) | ||
| Launch Weight (t) | 26.9 | |
| Fuel Weight (t) | ||
| Range (km) | ||
| CEP (m) (Russian Sources) | ||
| CEP (m) Western Sources) | ||
| Number of Stages | 2 | |
| Warheads Deployed | ||
| Booster guidance system | ||
| 1st stage | 2nd stage | |
| Length (m) | ||
| Body diameter (m) | ||
| Fueled weight (t) | ||
| Dry weight (t) | ||
| Engine Designation | ||
| Propellants | Solid | Solid |
| Fuel | ||
| Oxidizer | ||
| Burning time (s) | ||
| Verniers Thrust Sea Level/Vacuum (kn) | ||
| Specific Impulse (s) | ||
| Launching Technique | Underwater dry start | |
| Firing condition |
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