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 Aeroplane 2464 v 95 n 4 Nov 21 1958 p 748-58)
Argosy
Engineering
Engineering ; 187 , n 4845
1959
2 pages
Article (Journal)
English
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