RD-250

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The RD-250 is the base version of a dual-nozzle family of liquid-fuel rocket engines, burning a hypergolic mixture of unsymmetrical dimethylhydrazine (UDMH) 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 (8K67). 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.

1965  WikimediaWikidata
8D518
rocket engine



Желудочно-кишечный тракт Satan`ы - panoramioЖелудочно-кишечный тракт Satan`ы - panoramio
RD-250 rocket engineRD-250 rocket engine
    TypeSubtypeDateDescriptionNotesSource
    commonsimageЖелудочно-кишечный тракт Satan`ы - panoramio Commons
    commonsimageRD-250 rocket engine Commons