Weapons of Mass Destruction (WMD)
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 |
Sea state - Any weather
Submarine speed, kn
|
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