Cure cycle design methodology for fabricating reactive resin matrix fiber reinforced composites : a protocol for producing void-free quality laminates /

Bibliographic Details

Main Author:	Hou, T. H. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2014.
Series:	NASA technical memorandum ; 2014-218524.
Subjects:	Resin matrix composites. Laminates. Pressure distribution. Voids. Matrix materials. Polyimides.
Online Access:	https://purl.fdlp.gov/GPO/gpo54983 http://purl.fdlp.gov/GPO/gpo54983