RL-10A-1
From Spacefaring
model of rocket engine
Wikidata
LR115; RL10A-1
diameter 1.53 metre, specific impulse by weight 425 second, mass 131 kilogram, maximum thrust 66.7 kilonewton,
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, RL-10A, 1961,
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Location: KML, Cluster Map, Maps,
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