Account of redesign and development of Armstrong Siddeley turbojet; resulting Sa.6 has oa diam, 37.4 in.; oa length 134 in.; dry weight 2700 lb; minimum internal jet pipe diam, 22.6 in.; rated thrust 8000 lb at 8600 rpm; similar Sa.12 is rated 8500 lb thrust; reference to latest and most powerful Sapphire Sa.7 which differs considerably from Sa.6. (see also Flight v 69 n 2450 Jan 6 1956 p 17-22)


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    Titel :

    Sapphire series


    Weitere Titelangaben:

    Aeroplane


    Erschienen in:

    Aeroplane ; 89 , n 2307


    Erscheinungsdatum :

    1955


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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