AJ10-220

From Spacefaring




model of hypergolic rocket engine

Wikidata
AJ-10-220; Aerojet AJ10-220
length 19 centimetre, mass 1.95 kilogram, maximum thrust 62.3 newton, diameter 7.3 centimetre, specific impulse by weight 285 second, 
liquid propellant rocket engineAerojet Rocketdyne, 
United StatesAshkenazCalvinist Republic of GhentChinlandDemocratic Republic of the CongoHavilahKingdom of Martabam-hongsawatoiKingdom of WolaitaPersiaRemanSikh ConfederacySwedenTarshishDong Fang Hong 2Ekran


Location: KML, Cluster Map, Maps,


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