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Carbon/graphite fiber risk analysis and assessment study: An assessment of the risk to Douglas commercial transport aircraftThe potential hazard to electrical and electronic devices should there be a release of free carbon fibers due to an aircraft crash and fire was assessed. Exposure and equipment sensitivity data were compiled for a risk analysis. Results are presented in the following areas: DC-9/DC-10 electrical/electronic component characterization; DC-9 and DC-10 fiber transfer functions; potential for transport aircraft equipment exposure to carbon fibers; and equipment vulnerability assessment. Results reflect only a negligible increase in risk for the DC-9 and DC-10 fleets either now or projected to 1993.
Document ID
19800024980
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schjelderup, H. C.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Cook, C. Q.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Snyder, E.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Henning, B.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Hosford, J.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Gilles, D. L.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Swanstrom, C. W.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-159212
Report Number: NASA-CR-159212
Accession Number
80N33488
Funding Number(s)
CONTRACT_GRANT: NAS1-15508
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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