CL-44 has been completely redesigned and embodies United States materials, standards, processes and equipment; increases in design weights and fuselage volume, installation of Tyne engines and other major modifications; advantages of turboprop engines; direct and indirect operating costs given; airport compatibility; effect of mechanical loading on utilization and operating cost. (see also abstract in SAE -- J v 68 n 8 Aug 1960 p 91)
Canadair 44 -- Breakthrough cargo aircraft
SAE -- Paper
SAE Meeting ; 1960 Canadair
1960
24 pages
Conference paper
English
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Canadair 44 -- Breakthrough cargo aircraft
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