Study made of various propulsion and performance aspects of single-stage long range Mach 7 delta wing transport of 30,000 lb payload (125 passengers and cargo), encompasses consideration of propulsive performance of hypersonic ramjet design featuring lift augmentation; results indicate that 700,000-lb configuration could transport payload 3600 nautical mi with fuel reserve for descent and landing techniques similar to those presently used. (see also abstract in SAE -- J v 69 n 12 Dec 1961 p 47-53)
Feasibility of Mach 7 transport employing airbreathing propulsion systems
SAE -- Paper
SAE Meeting ; 1961 Supersonic
1961
35 pages
Conference paper
English
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Feasibility of Mach 7 transport employing airbreathing propulsion systems
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