AJ10-118F

From Spacefaring

Q135224760




model of hypergolic rocket engine

Wikidata
AJ-10-118F; Aerojet AJ10-118F
diameter 1.4 metre, maximum thrust 41.4 kilonewton, specific impulse by weight 306 second, mass 95 kilogram, 
liquid propellant rocket engineAerojet, United States
United StatesDong Fang Hong 2EkranRepublic of Haitiliquid propellant rocket engine


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource