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 GhentChinlandHavilahKingdom of Martabam-hongsawatoiKingdom of WolaitaPersiaRemanSikh ConfederacyTarshishDong Fang Hong 2EkranRepublic of Haitiliquid propellant rocket engine


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource