Q11833012: Difference between revisions

Latest revision as of 15:51, 17 February 2025

Soviet liquid rocket engine

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Wikidata
8D77
height 2.86 metre, diameter 0.67 metre, mass 1250 kilogram, specific impulse by weight 315 second, specific impulse by weight 246 second, maximum thrust 804 kilonewton, maximum thrust 628 kilonewton,
RD-108, 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-108, Republic of Haiti,

Location: KML, Cluster Map, Maps,

Type	Subtype	Date	Description	Notes	Source

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