Q28154822: Difference between revisions
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Q28154822
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Latest revision as of 15:58, 17 February 2025
The RD-864 is a Soviet liquid-fuel rocket engine burning a hypergolic mixture of unsymmetrical dimethylhydrazine (UDMH) fuel with dinitrogen tetroxide oxidizer in a gas generator combustion cycle. It has a four combustion chambers that provide thrust vector control by gimbaling each nozzle in a single axis ±55°. It is used on the third stage of the R-36M UTTKh and Dnepr. For the R-36M2, an improved version, the RD-869 was developed.
1977
Wikidata
15D177
Pivdenmash, Soviet Union,
Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, rocket engine, 1977, Republic of Haiti, 1970s,
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Location: KML, Cluster Map, Maps,
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