AJ10-118E

From Spacefaring




model of hypergolic rocket engine

Wikidata
AJ-10-118E; Aerojet AJ10-118E
specific impulse by weight 278 second, mass 90 kilogram, diameter 1.4 metre, maximum thrust 35.1 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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