| Characteristic |
Value |
| Maximum mass at the beginning, t |
4747 |
| Total mass of the 1st stage, t |
3593.6 |
| Mass of oxygen, t |
2230.4 |
| Mass of kerosene, t |
857.6 |
| Total mass of the 2nd stage, t |
934 |
| Mass of oxygen, t |
713 |
| Mass of hydrogen, t |
119 |
| Engine of the 1st stage (РД-179) |
|
| Thrust on the sea level, tf |
860 |
| Thrust in vacuum, tf |
937 |
| Engine of the 2nd stage (РД-0120) |
|
| Thrust on the sea level, tf |
175 |
| Thrust in vacuum, tf |
200 |
| Height, m |
88 |
| Dimensional specifications of the 1st stage |
|
| Height, m |
46.46 |
| Diameter, m |
3.92 |
| Dimensional specifications of the 2nd stage |
|
| Height, m |
63 |
| Diameter, m |
8 |
