6F-Polyhimides with phenylethynyl endcap for 315-370 ○C applications

被引:38
作者
Chuang, KC [1 ]
Bowman, CL
Tsotsis, TK
Arendt, CP
机构
[1] NASA, Glenn Res Ctr, Cleveland, OH 44135 USA
[2] Boeing Phantom Works, Huntington Beach, CA 94647 USA
关键词
Polyimides; phenylethynyl endcap; resin infusion; thermal cycling; rapid heating;
D O I
10.1177/0954008303015004005
中图分类号
O63 [高分子化学(高聚物)];
学科分类号
070305 ; 080501 ; 081704 ;
摘要
6F-Polyimides with a phenylethynyl endcap (HFPE) were fabricated into carbon fiber composites using the standard polymerization of monomer reactant (PMR) approach via the ester/acid route. T650-35/HFPE carbon fiber composites were evaluated against the corresponding T650-35/PMR-II-50 composites with nadic endcap at 315-370 degreesC (600-700 degreesF) for their physical and mechanical properties as well as thermo-oxidative stability In addition, concentrated HFPE monomer solutions were infused into stitched AS4 and T650-35 preforms and their mechanical properties were compared with those of the commercial BMI-5270 composites from cryogenic temperature to 343 degreesC (650 degreesF). The stitched HFPE composites out-performed BMI-5270 composites in terms of property retention at elevated temperature and microcrack resistance during thermal cycling from -54 to 288 degreesC (-65 to 550 degreesF). The stitched composites also showed more resistance toward blistering and delamination than conventional laminate composites during a rapid heating rate simulating launch and re-entry of reusable launch vehicles (RLV).
引用
收藏
页码:459 / 472
页数:14
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