RL-10B-2
From Spacefaring
model of rocket engine
1998
Wikidata
RL-10B-2-1; RL10B-2; RL10B-2-1
diameter 2.146 metre, length 4.15 metre, specific impulse by weight 465.5 second, mass 301 kilogram, maximum thrust 110 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-10, 1998, Republic of Haiti, 1990s,
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Location: KML, Cluster Map, Maps,
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