R-29RM / SS-N-23 SKIFF
| Specifications | |||
|---|---|---|---|
| DIA | SS-N-23 | SS-N-23 Mod 2 | SS-N-23 Mod 3 |
| NATO | SKIFF | ||
| Bilateral | RSM-54 | ||
| Service | R-29RM | R-29RMU | R-29RMU2 |
| Shtil [Shetal] | Sineva | Layner | |
| OKB/Industry | 3M37 | . | . |
| Design Bureau | KB Makeev | ||
| Approved | . | . | |
| Years of R&D | . | . | |
| Engineering and Testing | . | . | |
| First Flight Test | June 1983 | 2004 | 20 May 2011 |
| Deployment Date | 1986 | 2007 | 2014 |
| Guaranteed service life | . | 18-20 years | |
| Launch system | D-9RM with 16 missiles | ||
| Submarine | DELTA IV | ||
| Type of Warhead | MIRV | ||
| Warheads | 4 (tested with 10) | 10 |
|
| Yield | 100 kt | . | . |
| CEP (m) (Russian Sources) | 500 | . | 500 |
| CEP (m) Western Sources) | 500-900 meters | . | . |
| Payload (kg) | 2800 | . | 2800 |
| Total length (m) | 14.8 | ||
| Total length w/o warhead (m) | |||
| Missile Diameter (m) | 1.9 | ||
| Diameter of Stabilizers (m) | |||
| Launch Weight (t) | 40.3 | ||
| Fuel Weight (t) | |||
| Range (km) | 8300 | 8300 | |
| Number of Stages | 2 | 3 | |
| Warheads Deployed | |||
| Booster guidance system | astroinertial | ||
| Firing conditions | |||
| Sea State | |||
| Submarine speed, kn | |||
| Launching Technique | Underwater wet start/ surface |
Underwater wet start/ surface |
Underwater wet start/ surface |
| 1st stage | 2nd stage | 3nd stage | |
| Length (m) | |||
| Body diameter (m) | 1.9 | 1.9 | 1.85 |
| Fueled weight (t) | |||
| Dry weight (t) | |||
| Engine Designation | |||
| Propellants | Liquid | Liquid | Liquid |
| Fuel | Nitrogen Tetraoxide | Nitrogen Tetraoxide | Nitrogen Tetraoxide |
| Oxidizer | UDMH | UDMH | UDMH |
| Burning time (s) | |||
| Verniers Thrust Sea Level/ Vacuum (kn) |
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| Specific Impulse (s) |
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