Configuration Design and Recovery Considerations for a Staged SST

912232

09/01/1991

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
The design and recovery considerations are presented for a staged supersonic transport (SSST). It is shown that the SSST offers economic benefits over the conventional SST. The SSST benefits from the ability to “optimize” the design for minimum drag during supersonic cruise without the penalties of: landing gear, extensive flaps for landing, and the meeting of FAR 36 noise requirements. The recovery considerations are also presented to validate the SSST concept.
Meta TagsDetails
DOI
https://doi.org/10.4271/912232
Pages
19
Citation
Mills, N., Lawson, T., and Roskam, J., "Configuration Design and Recovery Considerations for a Staged SST," SAE Technical Paper 912232, 1991, https://doi.org/10.4271/912232.
Additional Details
Publisher
Published
Sep 1, 1991
Product Code
912232
Content Type
Technical Paper
Language
English