AJ10-118D

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Q135224758




model of hypergolic rocket engine

Wikidata
AJ-10-118D; Aerojet AJ10-118D
mass 90 kilogram, maximum thrust 33.7 kilonewton, diameter 0.84 metre, specific impulse by weight 278 second, 
liquid propellant rocket engineAerojet, United States
United StatesAshkenazCalvinist Republic of GhentChinlandDemocratic Republic of the CongoHavilahKingdom of Martabam-hongsawatoiKingdom of WolaitaPersiaRemanSikh ConfederacyTarshishDong Fang Hong 2EkranRepublic of Haitiliquid propellant rocket engine


Location: KML, Cluster Map, Maps,


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