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)
Sapphire series
Aeroplane
Aeroplane ; 89 , n 2307
1955
7 pages
Article (Journal)
English
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Engineering Index Backfile | 1956
Engineering Index Backfile | 1956
Engineering Index Backfile | 1956
British Library Online Contents | 1999
NTIS | 1998
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