Preliminary Sizing of a Supersonic Commercial Transport Between Mach 2.0 and 2.4

965589

10/01/1996

Event
World Aviation Congress & Exposition
Authors Abstract
Content
To review specifications of a next-generation supersonic commercial transport (SCT), conceptual design is performed. The study covers the cruise speed between Mach 2.0 and 2.4, and the range between 4,000 nmi and 6,000 nmi with the number of seats fixed to 300. Engines for Mach 2.0, 2.2 and 2.4 are conceptually designed and the data are applied to Japan Aircraft Development Corporation (JADC)'s SCT sizing and performance prediction tool (“CAD”). The maximum take off weights (MTOW) are surveyed to find the best combination of cruise speed and range.
Meta TagsDetails
DOI
https://doi.org/10.4271/965589
Pages
12
Citation
Takasu, T., Maekawa, S., Ugai, T., and Mizuno, H., "Preliminary Sizing of a Supersonic Commercial Transport Between Mach 2.0 and 2.4," SAE Technical Paper 965589, 1996, https://doi.org/10.4271/965589.
Additional Details
Publisher
Published
Oct 1, 1996
Product Code
965589
Content Type
Technical Paper
Language
English