Q16594359: Difference between revisions

Latest revision as of 15:53, 17 February 2025

Soviet liquid rocket engine

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Wikidata
8D76
mass 1155 kilogram, diameter 0.67 metre, height 2.86 metre, specific impulse by weight 252 second, specific impulse by weight 310 second, maximum thrust 789.2 kilonewton, maximum thrust 971 kilonewton,
RD-107, NPO Energomash, Soviet Union,
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, RD-107, Republic of Haiti,

Location: KML, Cluster Map, Maps,

Type	Subtype	Date	Description	Notes	Source

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