RD-0110R
The RD-0110R (GRAU Index 14D24) is a rocket engine burning liquid oxygen and kerosene in a gas generator combustion cycle. It has four nozzles that can gimbal up to 45 degrees in a single axis and is used as the vernier thruster on the Soyuz-2-1v first stage.[1] It also has 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 is supplied from the same LOX tank in liquid form, while the helium is supplied from separate high pressure bottles (known as the T tank).[1]
Country of origin | Russia |
---|---|
First flight | 2013-12-28 |
Designer | KBKhA,[1] Viktor Gorokhov[2] |
Manufacturer | Voronezh Mechanical Plant[2] |
Application | 1st stage vernier engine |
Associated L/V | Soyuz-2-1v[1] |
Predecessor | RD-0110[1] |
Status | In Production |
Liquid-fuel engine | |
Propellant | LOX[1] / RG-1[1] |
Cycle | Gas Generator[1] |
Configuration | |
Chamber | 4[1] |
Performance | |
Thrust (vac.) | 265.1 kilonewtons (59,600 lbf)[1] |
Thrust (SL) | 230.5 kilonewtons (51,800 lbf)[1] |
Chamber pressure | 6.6 megapascals (960 psi)[1] |
Isp (vac.) | 298.4 seconds[1] |
Isp (SL) | 259.4 seconds[1] |
Burn time | 210s[1] |
Dimensions | |
Length | 1,910 millimetres (75 in)[1] |
Diameter | 2,675 millimetres (105.3 in)[1] |
Dry weight | 850 kilograms (1,870 lb)[1] (including the support ring) |
Used in | |
Soyuz-2-1v first stage. |
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 TsSKB Progress. The RD-0110R engine is produced at the Voronezh Mechanical Plant.[2]
See also
- Soyuz-2-1v - The first rocket to use the RD-0110R
- KBKhA - The RD-0110R designer bureau
- RSC Progress - The designer of the Soyuz-2.1v and the RD-0110R nozzle gimbal
- Voronezh Mechanical Plant - A space hardware manufacturer company that manufactures the RD-0110R
References
- "Steering engine RD0110R (14D24). Carrier rocket "Soyuz-2-1v"" (in Russian). KBKhA. Retrieved 2015-06-01.
- Zak, Anatoly. "RD-0110R". russianspaceweb.com. Retrieved 2015-06-01.