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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