The RD-120 is intended for thrust creation needed for set-up a motion parameters transition to LV. It is used as cruise engine for Zenit LV second stage.
liquid oxygen + kerosene
|Vacuum thrust, tf||93|
|Vacuum specific propulsive burn, s||350,5|
|Propellant mixture ratio||2,6|
|Number of restarts||1|
|Gimbal angle of chambers||Stationary|
|Firing time, s||290|