RL-10A-4-1
From Spacefaring
Q31281954
Q31281954
model of rocket engine
2000
Wikidata
RL10A-4-1, RL-10A-4-1B, 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,
Persia, Republic of Haiti, 2000, RL-10A, Ekran, Dong Fang Hong 2, Tarshish, Sweden, Sikh Confederacy, United States, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz,
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Location: KML, Cluster Map, Maps,
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