| Length |
11.2 m
12.982 m ( estimated data)
|
| Case diameter |
1.36 meter. [estimated data]
3rd stage - 1.16 m ( estimated data *)
|
| Launch weight |
about 15000 kg (initial stage of the project)
about 17000 kg (final version of the project)
16838 kg ( estimated design data *)
|
| Throw Weight |
500 kg
530 kg ( estimated calculation data on Nikolaev *)
|
| Range |
10000-11000 km (estimated)
10,000 km ( estimates calculated data on Nikolaev *)
|
| CEP | not more than 350 m
|
| Motor run time | 120 s (estimated data for Nikolaev *)
|
| Operating temperature | from -40 to +50 ° C
|
| Wind speed at start | up to 25 m / s
|
| RV types | nuclear monoblock with a capacity of 100-150 kt (option - 0.5 Mt - estimated data *) , possibly with a set of means of overcoming missile defense.
|
| * Nikolaev Yu.M., Panin S.D. Basics of designing solid-propellant guided ballistic missiles (part 2). M., MSTU, 1998.
|
