RD-250
From Spacefaring
Q25346168
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
Wikimedia, Wikidata
8D518
Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, 1965,
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Location: KML, Cluster Map, Maps,
Желудочно-кишечный тракт Satan`ы - panoramio
RD-250 rocket engine| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Желудочно-кишечный тракт Satan`ы - panoramio | Commons | ||
| commons | image | RD-250 rocket engine | Commons | ||
