Q50101842: Difference between revisions
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Q50101842
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{{Page|Gamma 2|Classes|model of British rocket engine|Bristol Siddeley Gamma 2 | {{Page|Gamma 2|Classes|model of British rocket engine|Bristol Siddeley Gamma 2; Double Gamma}} | ||
Latest revision as of 12:46, 2 September 2025
model of British rocket engine
1969
Wikimedia, Wikidata
Bristol Siddeley Gamma 2; Double Gamma
mass 173 kilogram, diameter 1.37 metre, specific impulse by weight 251 second, specific impulse by weight 265 second, maximum thrust 64.6 kilonewton, maximum thrust 68.2 kilonewton,
Bristol Siddeley, United Kingdom,
Persia, Republic of Haiti, 1969, rocket engine, Ekran, Dong Fang Hong 2, Tarshish, Sweden, 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,
London2007more img 5550
Gamma 2 rocket engine on Black Arrow 2nd stage
Gamma 2 engine
Black Arrow 2nd stage engine| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | London2007more img 5550 | Commons | ||
| commons | image | Gamma 2 rocket engine on Black Arrow 2nd stage | Commons | ||
| commons | image | Gamma 2 engine | Commons | ||
| commons | image | Black Arrow 2nd stage engine | Commons | ||
