R-13 / SS-N-4 SARK
| Specifications | ||
|---|---|---|
| DIA | SS-N-4 | |
| NATO | Sark | |
| Bilateral | ||
| Service | R-13 | |
| OKB/Industry | 4K50 | |
| Design Bureau | SKB-385 | |
| Approved | ||
| Years of R&D | ||
| Engineering and Testing | 1959-1960 | |
| First Flight Test | 1959 | |
| IOC | ||
| Deployment Date | 10/13/1961 | |
| Launch system | D-2/D-3 | |
| Submarine | Golf & Hotel class | |
| Type of Warhead | Single | |
| Warheads | 1 | |
| Yield (mt) | 1 | |
| Payload (t) | 1.6 | |
| Total length (m) | 11.8 | |
| Total length w/o warhead (m) | ||
| Missile Diameter (m) | 1.3 | |
| Diameter of Stabilizers (m) | 1.9 | |
| Launch Weight (t) | 13.745 | |
| Fuel Weight (t) | ||
| Range (km) | 600 | |
| CEP (m) (Russian Sources) | 4,000 | |
| CEP (m) Western Sources) | 1,800 - 3,900 | |
| Number of Stages | 1 | |
| Warheads Deployed | ||
| Booster guidance system | ||
| Engine Designation | ||
| Propellants | Liquid | |
| Fuel | AK-27I | |
| Oxidizer | TG-02 | |
| Burning time (s) | ||
| Verniers Thrust Sea Level/Vacuum (kn) | ||
| Specific Impulse (s) | ||
| Launching Technique | Surfaced | |
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