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 |