RL-10C-1

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Q124651094




model of rocket engine

Wikidata
RL10C-1
mass 190.5 kilogram, maximum thrust 101.82 kilonewton, length 2.18 metre, diameter 1.45 metre, specific impulse by weight 449.7 second, 
RL-10CAerojet Rocketdyne, United States
United StatesAshkenazCalvinist Republic of GhentChinlandHavilahKingdom of Martabam-hongsawatoiKingdom of WolaitaPersiaSikh ConfederacyTarshishDong Fang Hong 2RL-10CRepublic of Haiti


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource