Q4386493: Difference between revisions
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Q4386493
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{{Page|RD-0410|Classes|}} | {{Page|RD-0410|Classes|Soviet nuclear thermal rocket engine|}} | ||
Latest revision as of 21:03, 24 October 2025
RD-0410 was a Soviet nuclear thermal rocket engine developed by the Chemical Automatics Design Bureau in Voronezh from 1965 through the 1980s using liquid hydrogen propellant. The engine was ground-tested at the Semipalatinsk Test Site, and its use was incorporated in the Kurchatov Mars 1994 crewed mission proposal.
Wikidata
Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, rocket engine, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
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