RL-10A-4

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Q31281953




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, 
RL-10A, Pratt & Whitney, United States, 
Sikh Confederacy, 1990s, Republic of Haiti, 1992, RL-10A, Ekran, Dong Fang Hong 2, Tarshish, Sweden, United States, Persia, 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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