AJ10-118E

From Spacefaring

Q135224759




model of hypergolic rocket engine

Wikidata
AJ-10-118E; Aerojet AJ10-118E
mass 90 kilogram, specific impulse by weight 278 second, maximum thrust 35.1 kilonewton, diameter 1.4 metre, 
liquid propellant rocket engineAerojet, United States
United StatesDong Fang Hong 2liquid propellant rocket engine


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource