NASA Technical Reports Server (NTRS) 19910009921: Effect Of Fiber Reinforcements On Thermo-oxidative Stability And Mechanical Properties Of Polymer Matrix Composites - Info and Reading Options
By NASA Technical Reports Server (NTRS)
"NASA Technical Reports Server (NTRS) 19910009921: Effect Of Fiber Reinforcements On Thermo-oxidative Stability And Mechanical Properties Of Polymer Matrix Composites" and the language of the book is English.
“NASA Technical Reports Server (NTRS) 19910009921: Effect Of Fiber Reinforcements On Thermo-oxidative Stability And Mechanical Properties Of Polymer Matrix Composites” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19910009921: Effect Of Fiber Reinforcements On Thermo-oxidative Stability And Mechanical Properties Of Polymer Matrix Composites
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
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- Internet Archive ID: NASA_NTRS_Archive_19910009921
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"NASA Technical Reports Server (NTRS) 19910009921: Effect Of Fiber Reinforcements On Thermo-oxidative Stability And Mechanical Properties Of Polymer Matrix Composites" Description:
The Internet Archive:
A number of studies have investigated the thermo-oxidative behavior of polymer matrix composites. Two significant observations have been made from these research efforts: (1) fiber reinforcement has a significant effect on composite thermal stability; and (2) geometric effects must be considered when evaluating thermal aging data. A compilation of some results from these studies is presented, and this information shows the influence of the reinforcement fibers on the oxidative degradation of various polymer matrix composites. The polyimide PMR-15 was the matrix material that was used in these studies. The control composite material was reinforced with Celion 6000 graphite fiber. T-40R graphite fibers, along with some very stable ceramic fibers were selected as reinforcing fibers because of their high thermal stability. The ceramic fibers were Nicalon (silicon carbide) and Nextel 312 (alumina-silica-boron oxide). The mechanical properties of the two graphite fiber composites were significantly different, probably owing to variations in interfacial bonding between the fibers and the polyimide matrix. The Celion 6000/PMR-15 bond is very tight but the T-40/PMR-15 bond is less tight. Three oxidation mechanisms were observed: (1) the preferential oxidation of the Celion 6000 fiber ends at cut surfaces, leaving a surface of matrix material with holes where the fiber ends were originally situated; (2) preferential oxidation of the composite matrix; and (3) interfacial degradation by oxidation. The latter two mechanisms were also observed on fiber end cut surfaces. The fiber and interface attacks appeared to initiate interfiber cracking along these surfaces.
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