Q4290405: Difference between revisions
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Q4290405
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{{Page|Gamma 8|Classes|model of British rocket engine}} | {{Page|Gamma 8|Classes|model of British rocket engine|Bristol Siddeley Gamma 8}} | ||
Latest revision as of 16:00, 17 February 2025
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,
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,
| Type | Subtype | Date | Description | Notes | Source |
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