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Carbon/graphite composite material study, appendix A and appendix BA comprehensive assessment of the possible damage to electrical and electronic equipment caused by accidental release of carbon fibers from burning civil aircraft with carbon composite parts was completed. The study concluded that the amount of fiber likely to be released is much lower than initially predicted. Carbon fiber released from an aircraft crash fire was found (from atmospheric dissemination models) to disperse over a much larger area than originally estimated, with correspondingly lower fiber concentrations. Long term redissemination of fiber was shown to be insignificant if reasonable care is exercised in accident cleanup. The vulnerability of electrical equipment to structural fibers in current use was low. Consumer appliances, industrial electronics, and avionics were essentially invulnerable to carbon fibers. Shock hazards (and thus potential injury or death) were found to be extremely unlikely.
Document ID
19810021651
Acquisition Source
Legacy CDMS
Document Type
Other
Date Acquired
August 11, 2013
Publication Date
January 15, 1981
Publication Information
Publication: Executive Office of the President Carbon(Graphite Composite Material Study
Subject Category
Composite Materials
Accession Number
81N30190
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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