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, 
Persia, Republic of Haiti, 2002, RL-10A, Ekran, Dong Fang Hong 2, Tarshish, Sweden, 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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