| RS-26 Rubezh
|
| Type | Intercontinental ballistic missile
|
| Country of origin | Russia
|
| Used by | Russian Strategic Missile Troops
|
| Designer | Moscow Institute of Thermal Technology
|
| Produced | 2011 ??
|
| Entered service | ?
|
| basing method | RGRK (mobile ground missile complex)
|
| Launch type | mobile launcher
|
| TEL Mobility |
|
| Engine | diesel
|
| Engine power | ?
|
| Maximum road speed | 45 km/h
|
| Range | 500 km
|
| TEL Dimensions |
|
| Weight | ~ 66.5 t
|
| Length | ~ 17 m
|
| Width | 3.4 m
|
| Height | ~ 4 m
|
| Missile Dimensions |
|
| Missile length | ~ 12 m ?? 20-22 m
|
| Missile diameter | ~ 1.8 m ?? 2-2.5 m
|
| Missile launch weight | 40 to 50 tons? ~ 36 t / 36,000 kilograms (80,000 lb)
|
| Number of stages | 3
|
| Motor | Solid-fueled (last stage or warhead block is liquid)
|
| Propellant | solid, warhead block probably liquid
|
| Operational range | 5800 km demonstrated
|
| Flight altitude | Several tens of km
|
| Maximum speed | over Mach 20 (24,500 km/h; 15,200 mph; 6.81 km/s)
|
| Guidance | Inertial [with GLONASS?]
|
| type of warhead | MIRV (multiple independent Reentry Vehicles)
|
| Throw weight | ~ 800-1500 kg
|
| Number of RVs | 1 / 4 / 6
|
| Warhead type | 1 x single nuclear warhead 550 kT yield
4 x MIRVs with 150-300 kT yield each (similar to RS-24 Yars)
6 x MIRVs
1 x Avangard hypersonic glide vehicle
|
| Accuracy | ? / 90-250 m CEP
|
