RL-10A-4-2

model of rocket engine

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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, Dong Fang Hong 2, RL-10A, 2002, 

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Location: KML, Cluster Map, Maps,

Type	Subtype	Date	Description	Notes	Source