Paper compares power plants from viewpoint of economic propulsion; method is based on mission analysis determining performance of aircraft with various engines installed; it is found that suitably optimized dry turbojet offers substantial size and range advantages for Mach 3 transports; such engines result in large installed thrust-to-weight ratios at takeoff, thus shortening runway requirements and improving initial climb rates.
Some aspects of supersonic transport propulsion
SAE -- Paper
SAE Meeting ; 1961
1961
4 pages
Conference paper
English
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