RL-10A-4-1
From Spacefaring
model of rocket engine
2000
Wikidata
RL-10A-4-1B; RL10A-4-1; RL10A-4-1B
maximum thrust 99.1 kilonewton, diameter 1.53 metre, specific impulse by weight 451 second, mass 167 kilogram,
Pratt & Whitney, 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-10A, 2000, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
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