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RD-0255
Soviet upper stage rocket engine From Wikipedia, the free encyclopedia
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The RD-0255 (Russian: Ракетный Двигатель-0255, romanized: Raketnyy Dvigatel-0255, lit. 'Rocket Engine 0255') is a propulsion module composed of an RD-0256 main engine and a RD-0257 Vernier thruster. Both are liquid-fuel rocket engines, burning a hypergolic mixture of unsymmetrical dimethylhydrazine (UDMH) fuel with dinitrogen tetroxide (N2O4) oxidizer. The RD-0256 main engine operates in the oxidizer rich staged combustion cycle, while the vernier RD-0257 uses the simpler gas generator cycle. It was used on the R-36MUTTKh (GRAU:15A18) and R-36M2 (GRAU:15A18M). Subsequently, it has been in the Dnepr second stage and as of 2016 it is still in active service.[4][5]
 | This article may require cleanup to meet Wikipedia's quality standards. The specific problem is: The article needs more scientific explanation. (February 2019) |
The RD-0256 is an improved version of the RD-0228 (GRAU: 15D84), itself composed of an RD-0229 (GRAU: 15D84) main engine and a RD-0230 (GRAU: 15D79) vernier engine.[6] The RD-0228 was developed between 1967 and 1974 for the first generation of R-36M (GRAU: 15D83) ICBM second stage, but was replaced on subsequent iterations by the RD-0256.[7] The RD-0228 debut was on January 21, 1973. With the START I and START II the RD-0228 was retired and its successor, the RD-0256, only continued as the Dnepr.[3][7]
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See also
- R-36M – A Soviet ICBM that used the RD-0228 and RD-0255.
- Dnepr – Small launch vehicle designed by Yuzhmash that uses the RD-0255.
- KBKhA – The RD-0228 and RD-0255 design bureau.
- Vernier Engine
- Rocket engine
References
External links
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