| 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:
- Sea state
- Submarine Speed, kn
|
|
| Deployed boosters |
|
| Test Boosters |
|
| Warheads Deployed |
|
| Training Launchers |
|
