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Full-scale aircraft cabin flammability tests of improved fire-resistant materialsFull-scale aircraft cabin flammability tests to evaluate the effectiveness of new fire-resistant materials by comparing their burning characteristics with those of older aircraft materials are described. Three tests were conducted and are detailed. Test 1, using pre-1968 materials, was run to correlate the procedures and to compare the results with previous tests by other organizations. Test 2 included newer, improved fire-resistant materials. Test 3 was essentially a duplicate of test 2, but a smokeless fuel was used. Test objectives, methods, materials, and results are presented and discussed. Results indicate that the pre-1968 materials ignited easily, allowed the fire to spread, produced large amounts of smoke and toxic combustion products, and resulted in a flash fire and major fire damage. The newer fire-resistant materials did not allow the fire to spread. Furthermore, they produced less, lower concentrations of toxic combustion products, and lower temperatures. The newer materials did not produce a flash fire.
Document ID
19740020310
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stuckey, R. N.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Surpkis, D. E.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Price, L. J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1974
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-58141
JSC-09060
Report Number: NASA-TM-X-58141
Report Number: JSC-09060
Accession Number
74N28423
Funding Number(s)
PROJECT: RTOP 501-38-19-01-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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