RL-10B-2

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Q31281957




model of rocket engine

1998  Wikidata
RL10B-2, RL-10B-2-1, 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, 
RL-10, Pratt & Whitney, United States, 
Persia, 1990s, Republic of Haiti, 1998, RL-10, Ekran, Dong Fang Hong 2, Tarshish, 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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