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The 737 aircraft flammability testingThe FAA requested approximately 20 component and full-scale tests in a 737 fuselage to provide validation data or indicate changes that need to be made to a fire math model (Dayton Aircraft Cabin Fire Model) developed for the FAA. Some preliminary tests were conducted to evaluate the adequacy of planned instrumentation. The objectives of the program were met in that it was verified that propagation of a fire could be determined from the sequential response of thermocouples located on a test specimen(such as a seat), and continuous weighing of the specimen during the test was accomplished. Two differenct techniques for measuring smoke density were found to be comparable.
Document ID
19790003859
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bricker, R. W.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1978
Publication Information
Publication: NASA. Ames Res. Center Conf. on Fire Resistant Mater. (FIREMEN)
Subject Category
Air Transportation And Safety
Accession Number
79N12030
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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