R-29R/R-2S / SS-N-18 STINGRAY
| Specifications | ||||
|---|---|---|---|---|
| Mod1 | Mod2 | Mod3 | ||
| DIA | SS-N-18 | SS-N-18 | SS-N-18 | |
| NATO | Stingray | Stingray | Stingray | |
| Bilateral | RSM-50 | RSM-50 | RSM-50 | |
| Service | R-29R | R-29R | R-29R | |
| OKB/Industry | 3M40 | |||
| Design Bureau | Makeyev | Makeyev | Makeyev | |
| Approved | ||||
| Years of R&D | 1973- | 1973- | 1973- | |
| Engineering and Testing | ||||
| First Flight Test | ||||
| IOC | ||||
| Deployment Date | 1979 | |||
| Launch system | D-9R | D-9R | D-9R | |
| Submarine | Delta III | Delta III | Delta III | |
| Type of Warhead | Single | MIRVed | MIRVed | |
| Warheads | 1 | 3 | 7 | |
| Yield (mt) | 0.450 | 0.2 | 0.1 | |
| Payload (t) | 1.6 | 1.6 | 1.6 | |
| Total length (m) | 14.1 | 14.1 | 14.1 | |
| Total length w/o warhead (m) | ||||
| Missile Diameter (m) | 1.8 | 1.8 | 1.8 | |
| Diameter of Stabilizers (m) | ||||
| Launch Weight (t) | 35.3 | 35.3 | 35.3 | |
| Fuel Weight (t) | ||||
| Range (km) | 8000 | 6500 | 6500 | |
| CEP (m) (Russian Sources) | 900 | 900 | 900 | |
| CEP (m) Western Sources) | ||||
| Number of Stages | 2 plus post boost vehicle | |||
| Warheads deployed | ||||
| Booster guidance system | Astroinertial | |||
| 1st stage | 2nd stage | |||
| Length (m) | ||||
| Body diameter (m) | ||||
| Fueled weight (t) | ||||
| Dry weight (t) | ||||
| Engine Designation | ||||
| Propellants | Liquid | |||
| Fuel | ||||
| Oxidizer | ||||
| Burning time (s) | ||||
| Verniers Thrust Sea Level/Vacuum (kn) | ||||
| Specific Impulse (s) | ||||
| Launching Technique | ||||
Firing conditions:
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| Deployed boosters | ||||
| Test Boosters | ||||
| Warheads Deployed | ||||
| Training Launchers | ||||
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