RT-15M
| Specifications | ||
|---|---|---|
| DIA | ||
| NATO | ||
| Bilateral | ||
| Service | RT-15M | |
| OKB/Industry | ||
| Design Bureau | SKB-385 | |
| Approved | ||
| Years of R&D | ||
| Engineering and Testing | ||
| First Flight Test | 1964 | |
| IOC | ||
| Deployment Date | Not deployed | |
| Launch system | D-7 | |
| Submarine | 667 Delta | |
| Type of Warhead | Single | |
| Warheads | 1 | |
| Yield (mt) | 1 | |
| Payload (t) | ||
| Total length (m) | 10.5 | |
| Total length w/o warhead (m) | ||
| Missile Diameter (m) | 1.5 | |
| Launch Weight (t) | 50 | |
| Fuel Weight (t) | ||
| Range (km) | 2400 | |
| CEP (m) (Russian Sources) | ||
| CEP (m) Western Sources) | ||
| Number of Stages | 2 | |
| Booster guidance system | Inertial autonomous | |
| 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 start | |
| Firing condition |
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