Weapons of Mass Destruction (WMD)
RT-2UTTH - Topol-M
SS-27
| Specifications
|
| DIA |
SS-27, SS-X-29, SS-25B |
| NATO |
|
| Bilateral |
RS-12M2 |
| Service |
RT-2PM2, RT-2PM-OS |
| OKB/Industry |
15Zh?? |
| Design Bureau |
(MIT)Moscow Institute of Thermal Technology |
| Approved |
2/ /1993 |
| Years of R&D |
1993 - 1997 |
| Engineering and Testing |
1994 1997 |
| First Flight Test |
12/20/94 |
| IOC |
1997 |
| Deployment Date |
12/27/1997 |
| Type of Warhead |
Single |
| Warheads |
1 |
| Yield (Mt) |
|
| Payload (t) |
1,000 - 1,200 |
| Total length (m) |
21.0 - 22.7 |
| Total length w/o warhead (m) |
17.9 |
| Missile Diameter (m) |
1.86 - 1.95 |
| Launch Weight (t) |
47.2 - 47.21 |
| Fuel Weight (t) |
|
| Range (km) |
10,000 -10,500 |
| CEP (m) (Russian Sources) |
|
| CEP (m) (Western Sources) |
350+ |
| Number of Stages |
3 |
| Canister length (m) |
21,2 - 23.0 |
Canister length w/o
front meters (m) |
19.44 |
| Canister diameter (m) |
2.0 |
| Booster guidance system |
Inertial, autonomous |
|
| 1st stage |
2nd stage |
3rd stage |
4th. BUS |
| Length (m) |
8.04? |
|
|
|
| Body diameter (m) |
1.86 - 1.95 |
1.61 |
1.58 |
|
| Fueled weight (t) |
28.6 |
|
|
|
| Dry weight (t) |
|
|
|
|
| Design Bureau for the Solid Motors |
MIT, NPO Soyuz |
MIT, NPO Soyuz |
MIT, NPO Soyuz |
|
| Engine Designation |
|
|
|
|
| Propellants |
Solid Propellant |
Solid Propellant |
Solid Propellant |
|
| Burning time (s) |
|
|
|
|
| Solid Motor Thrust Sea Level/Vacuum (Tonnes) |
|
|
|
|
| Specific Impulse (m/s) |
|
|
|
|
| Basing Mode |
Silo/Ground mobile |
| Hardness |
|
| Launching Technique |
|
| Deployed boosters |
|
| Test Boosters |
|
| Warheads Deployed |
|
| Deployment Sites |
|
| Training Launchers |
|
| Space Booster Variant |
No |
|
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