Powerplants for Future SSTs

760891

02/01/1976

Event
Aerospace Engineering and Manufacturing Meeting
Authors Abstract
Content
In further studies of Advanced Supersonic Transport (AST) powerplants the relative merits of several different engine cycles have been compared. The influence of the noise levels which have to be met is shown to be a dominant factor on the design of both the powerplant and the aircraft. An uprated turbofan derivative of the pure jet Olympus 593 Concorde engine could provide a satisfactory powerplant for a quiet and economically viable AST having improved pollution characteristics.
Meta TagsDetails
DOI
https://doi.org/10.4271/760891
Pages
17
Citation
Calder, P., and Gupta, P., "Powerplants for Future SSTs," SAE Technical Paper 760891, 1976, https://doi.org/10.4271/760891.
Additional Details
Publisher
Published
Feb 1, 1976
Product Code
760891
Content Type
Technical Paper
Language
English