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Bismaleimide resins for flame resistant honeycomb sandwich panelsBismaleimide resins are prime candidates for nonflammable aircraft interior panels. Three resin types with different structures and processing characteristics were formulated. Resin M 751 was used to fabricate 100 kg of glass fabric prepregs which were used for the preparation of face sheets for honeycomb sandwich panels. Prepreg characteristics and curing cycles for laminate fabrication are provided. In order to advance beyond the current solvent resin technology for fibre and fabric impregnation, a hot melt solvent-less resin system was prepared and characterized. Preliminary tests were performed to develop a wet bonding process for the fabrication of advanced sandwich honeycomb panels by use of polybismaleimide glass fabric face sheets and polybismaleimide Nomex honeycomb core. B-stage material was used for both the core and the face sheet, providing flatwise tensile properties equivalent to those obtained by the state-of-the-art 3-step process which includes an epoxy adhesive resin.
Document ID
19780022291
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stenzenberger, H. D.
(Technochemie G.m.b.H. Heidelberg, Germany)
Date Acquired
September 3, 2013
Publication Date
July 1, 1978
Subject Category
Nonmetallic Materials
Report/Patent Number
REPT-7807
NASA-CR-152206
Report Number: REPT-7807
Report Number: NASA-CR-152206
Accession Number
78N30234
Funding Number(s)
CONTRACT_GRANT: NASW-3081
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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