RL-10C-2-1

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Q124651097




model of rocket engine

Wikidata
RL10C-2-1
mass 301.2 kilogram, length 4.15 metre, diameter 2.15 metre, specific impulse by weight 465.5 second, maximum thrust 110.09 kilonewton, 
RL-10C, Aerojet Rocketdyne, United States, 
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, RL-10C, Republic of Haiti, 

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Location: KML, Cluster Map, Maps,


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