Gamma 2
From Spacefaring
model of British rocket engine
1969
Wikimedia, Wikidata
Bristol Siddeley Gamma 2; Double Gamma
diameter 1.37 metre, mass 173 kilogram, specific impulse by weight 251 second, specific impulse by weight 265 second, maximum thrust 64.6 kilonewton, maximum thrust 68.2 kilonewton,
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, 1969,
-
Location: KML, Cluster Map, Maps,
| 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 | ||



