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, 
Persia, 1960s, Republic of Haiti, 1969, rocket engine, Ekran, Dong Fang Hong 2, Tarshish, Sikh Confederacy, United Kingdom, 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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