Lyon, R. E. (1996). Fire Response of Geopolymer Structural Composites (Report No. DOT/FAA AR-TN95/22). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89534
Lyon, Richard E.. Fire Response of Geopolymer Structural Composites. Report no. DOT/FAA AR-TN95/22. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://rosap.ntl.bts.gov/view/dot/89534.
Lyon, Richard E. Fire Response of Geopolymer Structural Composites. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA AR-TN95/22, ROSA P. https://rosap.ntl.bts.gov/view/dot/89534.
The fire response of a potassium aluminosilicate matrix (geopolymer) carbon fiber composite was measured and the results compared to organic matrix composites being used for infrastructure and transportation applications. At irradiance levels of 50 kW/m2, typical of the heat flux in a well-developed fire, glass-or carbon-reinforced polyester, vinylester, epoxy, bismaleimde, cyanate ester, polyimide, phenolic, and engineering thermoplastic laminates ignited redly and released appreciable heat and smoke, while carbon-fiber reinforced geopolymer composites did not ignite, burn, or release any smoke even after extended heat flux exposure. The geopolymer matrix carbon fiber composite retains sixty-three percent of its original 245 MPa flexural strength after a simulated large fire exposure.
Lyon, R. E. (1996). Fire Response of Geopolymer Structural Composites (Report No. DOT/FAA AR-TN95/22). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89534
Lyon, Richard E.. Fire Response of Geopolymer Structural Composites. Report no. DOT/FAA AR-TN95/22. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://rosap.ntl.bts.gov/view/dot/89534.
Lyon, Richard E. Fire Response of Geopolymer Structural Composites. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA AR-TN95/22, ROSA P. https://rosap.ntl.bts.gov/view/dot/89534.
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