RL-10C-1-1

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Q124651095




model of rocket engine

Wikidata
length 2.46 metre, specific impulse by weight 453.8 second, mass 188.2 kilogram, diameter 1.57 metre, maximum thrust 105.98 kilonewton, 
RL-10CAerojet Rocketdyne, United States
United StatesAshkenazCalvinist Republic of GhentChinlandDemocratic Republic of the CongoHavilahKingdom of Martabam-hongsawatoiKingdom of WolaitaPersiaSikh ConfederacyTarshishDong Fang Hong 2EkranRL-10CRepublic of Haiti


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource