NASA NTRS ยท 19810021651
Carbon/graphite composite material study, appendix A and appendix B
Abstract
A 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.
Keep this discovery
Explore connections, maps & timelines
1981-01-15. Carbon/graphite composite material study, appendix A and appendix B. https://ntrs.nasa.gov/citations/19810021651
Cite the original work for its findings. Save a collection to share your selection of sources.