| Project Kaban Mursk |
| Type | Small Lift Launch Vehicle |
| Stage | 1 |
| Displacement | 125 t |
| Length | 25 m |
| Diameter | 3 m |
| Propellant | Kerosene Liquid Oxygen |
| Payload | LEO - 1.5t |
| First Stage |
| Engine | KE-2(SL) x 2 |
| Thrust | 1,500 kN |
| Propellant | RP-1 / LOX |
| Specific impulse | 250s |
| Burn Time | 310s |
