| Specifications |
| |
Mod1 |
Mod2 |
| DIA |
SS-N-8 |
SS-N-8 |
| NATO |
Sawfly |
Sawfly |
| Bilateral |
RSM-40 |
RSM-40 |
| Service |
R-29 |
R-29 |
| OKB/Industry |
4K75 |
|
| Design Bureau |
SKB-385 |
SKB-385 |
| Approved |
|
|
| Years of R&D |
|
|
| Engineering and Testing |
|
|
| First Flight Test |
|
|
| IOC |
|
|
| Deployment Date |
3/12/1974 |
1978 |
| Launch system |
D-9 with 12 missiles |
D-9D with 16 missiles |
| Submarine |
Delta I |
Delta I & Delta II |
| Type of Warhead |
|
|
| Warheads |
Single |
|
| Yield (Russian sources) |
|
|
| Yield (Western sources) |
0.6-1.5 MT |
0.6-1.5 MT |
| Payload (t) |
1.1 |
1.1 |
| Total length (m) |
13 |
|
| Total length w/o warhead (m) |
|
|
| Missile Diameter (m) |
1.8 |
|
| Diameter of Stabilizers (m) |
|
|
| Launch Weight (t) |
33.3 |
|
| Fuel Weight (t) |
|
|
| Range (km) |
7,800 |
9,100 |
| CEP (m) (Russian Sources) |
1,500 |
900 |
| CEP (m) Western Sources) |
900 |
900 |
| Number of Stages |
2 |
| 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 |
Liquid |
| Fuel |
|
|
| Oxidizer |
|
|
| Burning time (s) |
|
|
| Verniers Thrust Sea Level/Vacuum (kn) |
|
|
| Specific Impulse (s) |
|
|
| Launching Technique |
Underwater "wet start"/surfaced |
| Firing conditions:
|
Sea state - Any conditionUp to 5
Submarine Speed, kn --
|
