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Development of fiber shields for engine containmentTests were conducted in translational launchers and spin pits to generate empirical data used in the design of a Kevlar shield for containing engine burst debris. Methods are given for modeling the relationship of fragment characteristics to shielding requirements. The change in relative importance of shield mounting provisions as fragment energy is increased is discussed.
Document ID
19780002136
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bristow, R. J. (Boeing Co. Seattle, WA, United States)
Davidson, C. D. (Boeing 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
78N10079
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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