RD-0236

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RD-0236 (РД-0236)
Country of origin USSR
First flight 1973-04-09[1]
Designer OKB-154[1]
Application Vernier engine
Associated L/V UR-100N, Rokot and Strela[1]
Status Out of Production
Liquid-fuel engine
Propellant N2O4[1] / UDMH[1]
Cycle Gas Generator[1]
Configuration
Chamber 4[2]
Performance
Thrust 15.76 kilonewtons (3,540 lbf)[2]
Isp (vac.) 293 s (2.87 km/s)[2]
Used in
UR-100N second stage[2]

The RD-0236 (GRAU Index 15D114) is a liquid rocket vernier engine, burning N2O4 and UDMH in the gas generator cycle.[3][1] 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.[2] While the engine is out of production, the ICBM as well as Rokot and Strela remain operational as of 2015.[4]

See also

References

  1. ↑ 1.0 1.1 1.2 1.3 1.4 1.5 1.6 Lua error in package.lua at line 80: module 'strict' not found.
  2. ↑ 2.0 2.1 2.2 2.3 2.4 Lua error in package.lua at line 80: module 'strict' not found.
  3. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  4. ↑ Lua error in package.lua at line 80: module 'strict' not found.

External links

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