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Preliminary properties of a resin from ethynyl terminated materialsA blend composed of an ethynyl terminated aspartimide (brittle component) and an ethynyl terminated arylene ether oligomer (tough component) was thermally cured to yield a resin which underwent preliminary evaluation to determine the potential for use in structural applications on aerospace vehicles. The blend exhibited good compression moldability, allowing for fabrication of neat moldings, adhesive specimens and composites at temperatures of 250 C under a pressure of 1.4 MPa (200 psi). Neat resin moldings and adhesive specimens provided relatively high mechanical properties. Composite specimens provided promising results in spite of fiber misalignment, fiber washout, and a small amount of panel warpage.
Document ID
19930021653
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hergenrother, Paul M.
(NASA Langley Research Center Hampton, VA, United States)
Connell, John W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: First NASA Advanced Composites Technology Conference, Part 2
Subject Category
Composite Materials
Accession Number
93N30842
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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