RL-10C-1-1
From Spacefaring
model of rocket engine
Wikidata
RL10C-1-1
length 2.46 metre, specific impulse by weight 453.8 second, mass 188.2 kilogram, diameter 1.57 metre, maximum thrust 105.98 kilonewton,
Aerojet Rocketdyne, United States,
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, RL-10C, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
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