RL-10C-1

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Q124651094




model of rocket engine

Wikidata
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-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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