Gamma 8

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Q4290405




model of British rocket engine

1969  Wikimedia, Wikidata
Bristol Siddeley Gamma 8
mass 342 kilogram, diameter 1.98 metre, maximum thrust 222.4 kilonewton, maximum thrust 234.8 kilonewton, specific impulse by weight 265 second, specific impulse by weight 251 second, 
rocket engine, Bristol Siddeley, United Kingdom, 
United Kingdom, Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, rocket engine, 1969, Republic of Haiti, 1960s, 

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Location: KML, Cluster Map, Maps,


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