RL-10A-4-2

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Q31281955




model of rocket engine

2002  Wikidata
RL10A-4-2
mass 167.8 kilogram, diameter 1.53 metre, length 2.29 metre, specific impulse by weight 451 second, maximum thrust 99.2 kilonewton, 
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, 2002, Republic of Haiti, 

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Location: KML, Cluster Map, Maps,


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