AJ10-118

From Spacefaring

Q135224757




model of hypergolic rocket engine

Wikidata
AJ-10-118; Aerojet AJ10-118; Aerojet LR52-AJ-1; LR52-AJ-1
diameter 0.84 metre, specific impulse by weight 271 second, maximum thrust 33.8 kilonewton, mass 90 kilogram, 
liquid propellant rocket engineAerojet, United States
United StatesDong Fang Hong 2Ekranliquid propellant rocket engine


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource