High Temperature Materials for Aerospace Applications
Further crosslinking of the fluorinated polyimide was examined to separate the cure reactions from degradation and to determine the optimum post curing conditions. Glass transition/melting temperatures were ascertained using DSC, while weight loss during curing and Td were determined using TGA. Furt...
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| Format: | Others |
| Language: | en_US |
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2011
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| Online Access: | http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7828 |