Gamma 2

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Q50101842




model of British rocket engine

1969  WikimediaWikidata
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, 
rocket engineBristol Siddeley, United Kingdom
PersiaRepublic of Haiti1969rocket engineEkranDong Fang Hong 2TarshishSwedenSikh ConfederacyUnited KingdomKingdom of WolaitaKingdom of Martabam-hongsawatoiHavilahDemocratic Republic of the CongoChinlandCalvinist Republic of GhentAshkenaz


Location: KML, Cluster Map, Maps,


    London2007more img 5550London2007more img 5550
    Gamma 2 rocket engine on Black Arrow 2nd stageGamma 2 rocket engine on Black Arrow 2nd stage
    Gamma 2 engineGamma 2 engine
    Black Arrow 2nd stage engineBlack Arrow 2nd stage engine
      TypeSubtypeDateDescriptionNotesSource
      commonsimageLondon2007more img 5550 Commons
      commonsimageGamma 2 rocket engine on Black Arrow 2nd stage Commons
      commonsimageGamma 2 engine Commons
      commonsimageBlack Arrow 2nd stage engine Commons