Armstrong Whitworth (Aircraft) Ltd, powered by four 2100-hp Rolls-Royce Dart turboprops; fuselage freight hold has 10-ft wide floor, 4 ft from ground for loading from truck; freight hold is 6 ft 8 in. high; main wing structure in five sections is of two-spar type with 10 bag type fuel tanks between spars; estimates indicate that it will be able to take maximum no-reserves payload of 28,000 lb over 600 nautical mi. (see also Engineering v 187 n 4845 Jan 16 1959 p 74-75)
Argosy
Aeroplane
Aeroplane and Astronautics ; 95 , n 4
1958
11 pages
Article (Journal)
English
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Engineering Index Backfile | 1959
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