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 SAE -- Paper 427C for meeting Oct 9-13 1961 35 p)
Feasibility of Mach 7 transport employing airbreathing propulsion systems
SAE -- J
Society of Automotive Engineers -- Journal ; 69 , n 12
1961
7 pages
Aufsatz (Zeitschrift)
Englisch
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Feasibility of Mach 7 transport employing airbreathing propulsion systems
Engineering Index Backfile | 1961
|The Feasibility of a Mach 7 Transport Employing Airbreathing Propulsion Systems
SAE Technical Papers | 1961
|Springer Verlag | 2007