RD-250
The RD-250 is the base version of a dual-nozzle family of liquid-fuel rocket engines, burning a hypergolic mixture of unsymmetrical dimethylhydrazine fuel with dinitrogen tetroxide oxidizer in a gas-generator open cycle. The RD-250 was developed by OKB-456 for Yangel's PA Yuzhmash ICBM, the R-36. Its variations were also used on the Tsyklon-2 and Tsyklon-3 launch vehicles. It was supposed to be used on the Tsyklon-4, but since the cancellation of the project it should be considered as out of production.
Versions
The engine has seen different versions made:- RD-250 : Base engine of the family. Used on the R-36. A bundle of three RD-250 form the RD-251 cluster.
- RD-250P : Improved version of the RD-250. Used on the R-36P. A bundle of three RD-250P form the RD-251P cluster.
- RD-250M : Improved version of the RD-250P. Used on the R-36-O. A bundle of three RD-250M form the RD-251M cluster.
- RD-250PM : Improved version of the RD-250M. Used on the Tsyklon-3. A bundle of three RD-250PM form the RD-261 cluster.
- RD-252 : Vacuum optimized version of the RD-250. Used on the R-36 and Tsyklon-2 second stages.
- RD-262 : Improved version of the RD-252. Used on the Tsyklon-3 second stages.
Modules
- RD-251 : A module comprising three RD-250. Propulsion module of the R-36 first stage.
- RD-251P : A module comprising three RD-250P. Propulsion module of the R-36P first stage.
- RD-251M : A module comprising three RD-250M. Propulsion module of the R-36-O and Tsyklon-2 first stage.
- RD-261 : A module comprising three RD-250PM. Propulsion module of the Tsyklon-3 first stage.
Comparison