AJ10-118F

From Spacefaring




model of hypergolic rocket engine

Wikidata
AJ-10-118F; Aerojet AJ10-118F
diameter 1.4 metre, mass 95 kilogram, specific impulse by weight 306 second, maximum thrust 41.4 kilonewton, 
liquid propellant rocket engine
United StatesAshkenazCalvinist Republic of GhentChinlandDemocratic Republic of the CongoHavilahKingdom of Martabam-hongsawatoiKingdom of WolaitaPersiaRemanSikh ConfederacySwedenTarshishDong Fang Hong 2Ekran


Location: KML, Cluster Map, Maps,


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