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Engine non-containment: UK risk assessment methodsMore realistic guideline data must be developed for use in aircraft design in order to comply with recent changes in British civil airworthiness requirements. Unrealistically pessimistic results were obtained when the methodology developed during the Concorde SST certification program was extended to assess catastrophic risks resulting from uncontained engine rotors.
Document ID
19780002129
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wallin, J. C. (British Aircraft Corp. (Operating) Ltd. Bristol, United Kingdom)
Date Acquired
August 9, 2013
Publication Date
March 1, 1977
Publication Information
Publication: MIT An Assessment of Technol. for Turbojet Engine Rotor Failures
Subject Category
Aircraft Propulsion And Power
Accession Number
78N10072
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19780002125Collected WorksAn Assessment of Technology for Turbojet Engine Rotor Failures
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