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Development of assembly techniques for fire resistant aircraft interior panelsTen NASA Type A fire resistant aircraft interior panels were fabricated and tested to develop assembly techniques. These techiques were used in the construction of a full scale lavatory test structure for flame propagation testing. The Type A panel is of sandwich construction consisting of Nomex honeycomb filled with quinone dioxime foam, and bismaleimide/glass face sheets bonded to the core with polyimide film adhesive. The materials selected and the assembly techniques developed for the lavatory test structure were designed for obtaining maximum fire containment with minimum smoke and toxic emission.
Document ID
19810009573
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lee, S. C. S.
(HITCO Gardena, CA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1978
Subject Category
Composite Materials
Report/Patent Number
HTR-5-78
NASA-CR-152119
Report Number: HTR-5-78
Report Number: NASA-CR-152119
Accession Number
81N18097
Funding Number(s)
CONTRACT_GRANT: NAS2-9153
PROJECT: RTOP 510-56-01-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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