Comet 4 will have all-up weight of 152,500 lb and has four Avon engines of 10,500 lb thrust; capacity payload of first class version is 16,500 lb (60 passengers), and that of tourist version, 19,300 lb (76 passengers); structural design test program; factors in favor of wing engine installation; control system. (see also Flight v 69 n 2469 May 18 1956 p 607-9)
Comet 4 -- Design and operational considerations
Can Aeronautical J
Canadian Aeronautical Journal ; 2 , n 6
1956
10 pages
Aufsatz (Zeitschrift)
Englisch
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Comet 4 -- Design and operational considerations
Engineering Index Backfile | 1956
|Design considerations for operational readiness
AIAA | 1965
|AIAA | 2019
|Wiley | 2010
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