RL-10A-1

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Q31281949




model of rocket engine

1961  Wikidata
LR115, RL10A-1
diameter 1.53 metre, specific impulse by weight 425 second, maximum thrust 66.7 kilonewton, mass 131 kilogram, 
RL-10A, Pratt & Whitney, United States, 
Persia, 1960s, Republic of Haiti, 1961, RL-10A, 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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