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Rotor burst protection criteria and implicationsCurrent aircraft design practices to minimize the hazard from rotor bursts are described. The consequences of non-contained engine failures and the impact of rotor burst protection systems on aircraft design are discussed.
Document ID
19780002128
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mccormick, R. B. (Boeing Commercial Airplane Co. Seattle, WA, United States)
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
78N10071
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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