RD-0110R

RD-0110R
The four nozzles of the RD-0110R surround the large single nozzle of the NK-33 engine on the first stage of the Soyuz-2.1v.
Country of originRussia
First flight2013-12-28
DesignerKBKhA, Viktor Gorokhov
ManufacturerVoronezh Mechanical Plant
Application1st stage vernier engine
Associated LVSoyuz-2.1v
PredecessorRD-0110
StatusRetired
Liquid-fuel engine
PropellantLOX / RG-1
CycleGas-generator
Configuration
Chamber4
Performance
Thrust, vacuum265.1 kN (59,600 lbf)
Thrust, sea-level230.5 kN (51,800 lbf)
Chamber pressure6.6 MPa (960 psi)
Specific impulse, vacuum298.4 s (2.926 km/s)
Specific impulse, sea-level259.4 s (2.544 km/s)
Burn time210 seconds
Dimensions
Length1,910 mm (75 in)
Diameter2,675 mm (105.3 in)
Dry mass850 kg (1,870 lb) including the support ring
Used in
Soyuz-2.1v first stage

The RD-0110R (Russian: Ракетный Двигатель-0110Р (Р - рулевой), romanized: Raketnyy Dvigatel-0110R, lit.'Rocket Engine 0110R (R - rulevoy, steering)', GRAU index: 14D24) was a rocket engine burning kerosene in liquid oxygen in a gas generator combustion cycle. It had four nozzles that can gimbal up to 45 degrees in a single axis and was used as the vernier thruster on the Soyuz-2.1v first stage. It also had heat exchangers that heat oxygen and helium to pressurize the LOX and RG-1 tanks of the Soyuz-2.1v first stage, respectively. The oxygen was supplied from the same LOX tank in liquid form, while the helium was supplied from separate high pressure bottles (known as the T tank).

The engine's development started in 2010 and it is a heavily modified version of the RD-0110. The main areas of work were shortening the nozzles to optimize them for the atmospheric part of the flight (the RD-0110 is a vacuum optimized engine), propellant piping, heat exchangers and the gimballing system, which was developed by RKTs Progress. The RD-0110R engine was produced at the Voronezh Mechanical Plant.