Configuration Design and Recovery Considerations for a Staged SST

Paper #:
  • 912232

Published:
  • 1991-09-01
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.
Pages:
19
Abstract:
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.
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