AJ10-118

From Spacefaring




model of hypergolic rocket engine

Wikidata
AJ-10-118; Aerojet AJ10-118; Aerojet LR52-AJ-1; LR52-AJ-1
specific impulse by weight 271 second, maximum thrust 33.8 kilonewton, diameter 0.84 metre, mass 90 kilogram, 
liquid propellant rocket engine
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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