|Country of origin||USSR|
|Associated LV||UR-100N, Rokot and Strela|
|Status||Out of Production|
|Propellant||N2O4 / UDMH|
|Thrust||15.76 kilonewtons (3,540 lbf)|
|Specific impulse (vacuum)||293 s (2.87 km/s)|
|UR-100N second stage|
The RD-0236 (GRAU Index 15D114) is a liquid rocket vernier engine, burning N2O4 and UDMH in the gas generator cycle. It is used along the RD-0235 main engine on the UR-100UTTKh second stage. Its function is to supply thrust vector control by gimbaling each of its four nozzles in a plane. While the engine is out of production, the ICBM as well as Rokot and Strela remain operational as of 2015.