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 origin | Russia | 
|---|---|
| First flight | 2013-12-28 | 
| Designer | KBKhA, Viktor Gorokhov | 
| Manufacturer | Voronezh Mechanical Plant | 
| Application | 1st stage vernier engine | 
| Associated LV | Soyuz-2.1v | 
| Predecessor | RD-0110 | 
| Status | Retired | 
| Liquid-fuel engine | |
| Propellant | LOX / RG-1 | 
| Cycle | Gas-generator | 
| Configuration | |
| Chamber | 4 | 
| Performance | |
| Thrust, vacuum | 265.1 kN (59,600 lbf) | 
| Thrust, sea-level | 230.5 kN (51,800 lbf) | 
| Chamber pressure | 6.6 MPa (960 psi) | 
| Specific impulse, vacuum | 298.4 s (2.926 km/s) | 
| Specific impulse, sea-level | 259.4 s (2.544 km/s) | 
| Burn time | 210 seconds | 
| Dimensions | |
| Length | 1,910 mm (75 in) | 
| Diameter | 2,675 mm (105.3 in) | 
| Dry mass | 850 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.