RL-10A-4-1

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Q31281954




model of rocket engine

2000  Wikidata
maximum thrust 99.1 kilonewton, diameter 1.53 metre, specific impulse by weight 451 second, mass 167 kilogram, 
RL-10A, Pratt & Whitney, United States, 
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, RL-10A, 2000, Republic of Haiti, 

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Location: KML, Cluster Map, Maps,


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