RL-10A-4
From Spacefaring
model of rocket engine
1992
Wikidata
RL10A-4
diameter 1.17 metre, height 2.29 metre, specific impulse by weight 449 second, mass 168 kilogram, maximum thrust 92.5 kilonewton,
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, 1992, Republic of Haiti, 1990s,
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Location: KML, Cluster Map, Maps,
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