R-21 / SS-N-5 SERB
| Specifications | ||
|---|---|---|
| DIA | SS-N-5 | |
| NATO | Sark | |
| Bilateral | ||
| Service | ||
| OKB/Industry | 4K55 | |
| Design Bureau | OKB-586/SKB-385 | |
| Approved | ||
| Years of R&D | ||
| Engineering and Testing | ||
| First Flight Test | 2/24/1962 | |
| IOC | ||
| Deployment Date | 15/5/1963 | |
| Launch system | D-4 with 3 missiles | |
| Submarine | Golf-II / Hotel II | |
| Warheads | 1 | |
| Yield | 0.8-1.0 MT - Russian sources 2.0-3.5 MT - Western sources |
|
| Payload (kg) | 1,200 | |
| Total length (m) | 12.9-14.3 | |
| Total length w/o warhead (m) | ||
| Missile Diameter (m) | 1.3-1.4 | |
| Diameter of Stabilizers (m) | ||
| Launch Weight (t) | 16.6-19.7 | |
| Fuel Weight (t) | ||
| Range (km) | 1400 | |
| CEP (m) (Russian Sources) | 2,800 | |
| CEP (m) Western Sources) | 1,800 - 3,900 | |
| Number of Stages | 1 | |
| Warheads deployed | ||
| Booster guidance system | Inertial | |
| Engine Designation | ||
| Propellants | Liquid | |
| Fuel | ||
| Oxidizer | ||
| Burning time (s) | ||
| Verniers Thrust Sea Level/Vacuum (kn) | ||
| Specific Impulse (s) | ||
| Launching Technique | Underwater | |
| Firing conditions: |
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