Q25346168: Difference between revisions
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{{Page|RD-250|Classes|model of Ukrainian rocket engine}} | {{Page|RD-250|Classes|model of Ukrainian rocket engine|8D518}} | ||
Latest revision as of 15:57, 17 February 2025
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, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, rocket engine, 1965, Republic of Haiti,
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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 | ||
