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FAA Concept in Safety for the SST
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English
Abstract
This paper presents the airworthiness and operational standards approaches toward assuring a high level of safety for the supersonic transport. A description is given of the major technical problems and the means established for their resolution.
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Citation
Sliff, R., "FAA Concept in Safety for the SST," SAE Technical Paper 660293, 1966, https://doi.org/10.4271/660293.Also In
References
- “A Preliminary Study of Airworthiness for Operation and Maintenance.” FAA March 1961
- “Tentative Airworthiness Objectives and Standards for Supersonic Transport Design Proposals.” FAA August 1963
- Bray, Richard S. “A Piloted Simulator Study of Longitudinal Handling Qualities of Supersonic Transports in the Landing Maneuver.” NASA TN D-2251 Ames Research Center April 1964
- Powers Bruce G. Matheny, Keil W. “Flight Evaluation of Three Techniques of Demonstrating the Minimum Flying Speed of a Delta Wing Airplane.” NASA TN D-2337 Flight Research Center, Edwards Calif. July 1964
- Tymczyszyn J. J. Spiess, P. C. “The Effects of Supersonic Transport Flight Characteristics of Performance Requirements.” Paper 674D presented at SAE National Aeronautic Meeting, Washington, D. C. April 1963
- “Tentative Aiworthiness Standards for the Supersonic Transport.” FAA November 1965