RD-182 (120M)
Glavkosmos
Modification of the RD120 liquid-propellant rocket engine with afterburning of oxidizing gas for the first stages. Fuel: oxygen + kerosene. A number of new technologies are widely used in engine design. The development of the RD182 engine is a terrestrial modification of the RD120MS with a short noz
Technical specifications
- Thrust, earth / void, tf
- 79/89
- Specific impulse, earth / void, s
- 298/336
- Pressure in the combustion chamber, kgf / cm2
- 181,6
- Weight, dry / dipped, kg
- 1150/1260
- Dimensions height / diameter, mm
- 3653/2600
- Development period
- 2019-2022
- Thrust vector control (2 channels) due to camera swing in two planes, o
- 6
- Thrust range,%
- 100-50
About
Modification of the RD120 liquid-propellant rocket engine with afterburning of oxidizing gas for the first stages. Fuel: oxygen + kerosene. A number of new technologies are widely used in engine design. The development of the RD182 engine is a terrestrial modification of the RD120MS with a short nozzle for promising LV.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
