AJ10-220

From Spacefaring

Q135011331




model of hypergolic rocket engine

Wikidata
AJ-10-220; Aerojet AJ10-220
maximum thrust 62.3 newton, specific impulse by weight 285 second, diameter 7.3 centimetre, length 19 centimetre, mass 1.95 kilogram, 
liquid propellant rocket engineAerojet Rocketdyne, United States
United StatesDong Fang Hong 2EkranRepublic of Haitiliquid propellant rocket engine


Location: KML, Cluster Map, Maps,


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