AJ10-118K

From Spacefaring




model of hypergolic rocket engine

1982 — 2018  Wikimedia, Wikidata
AJ-10-118K; Aerojet AJ10-118K; Aerojet Rocketdyne AJ10-118K
specific impulse by weight 320.5 second, length 2.68 metre, mass 275 kilogram, diameter 1.53 metre, maximum thrust 43.38 kilonewton, 
liquid propellant rocket engine, 
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, 1982, 

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Location: KML, Cluster Map, Maps,


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