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Development of Design Data for Propulsion PMR-15 CompositesThe continuing development of PMR-15 composite materials and their associated design properties is pacing the implementation of this technology on commercial aircraft. The guidelines that the FAA has issued regarding the certification of advanced composite structures are very significant with respect to future PMR-15 research and development activities. The FAA has issued an advisory circular dated 1-5-83 concerning guidelines for composite aircraft structures. Of particular significance to PMR-15 technology development is the reliance on combined environmental exposure and component testing, coupled with the stipulation that reliance on previous experience be limited to where common structures and materials have been used for a similar function. Critical environmental exposures for commercial propulsion structures include 50,000 cycle service life, exposure to skydrol, moisture and other fluids, and nacelle fire conditions.
Document ID
19860001818
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Postlewaite, J.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Mclaren, D.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1985
Publication Information
Publication: NASA. Lewis Research Center High Temp. Polymer Matrix Composites
Subject Category
Composite Materials
Accession Number
86N11285
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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