(Contact Us for further information on the materials listed below or any other Barrday products)
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Description |
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High temperature semi-crystalline polymer with low moisture absorption and Tg of 200° F (95° C)
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Very high temperature semi-crystalline polymer with good combination of toughness, chemical solvent resistance, low moisture absorption, and FST properties. Tg of 289° F (143° C)
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Same benefits as PEEK with a wider and lower temperature processing window. Tg of 303° F (151° C) |
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Very high temperature semi-crystalline polymer with good combination of toughness, chemical solvent resistance, low moisture absorption, and FST properties. Tg of 319° F (159° C)
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High temperature tough amorphous polymer with excellent FST properties. |
Semi-crystalline polymer with good combination of strength, toughness, chemical and solvent resistance.
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Product |
Description |
Toughened epoxy prepreg system suitable for autoclave, press or bag molding operations. Fire retardant per FAR 25.833. Tg of 300° F (150° C)
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Toughened, low heat release epoxy prepreg system (Sub 30/30 OSU). Self-adhesive to honeycomb. Excellent surface finish. EPM503-1 is offered as a press grade system. REACH compliant.
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Toughened, low heat release epoxy prepreg system (Sub 40/40 OSU). Self-adhesive to honeycomb. Excellent surface finish. EPM505 is designed for bag molding. REACH compliant.
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High temperature curing, fire retardant epoxy per FAR 25.833. Excellent combination of toughness and high Tg of 300°F (150° C)
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Product |
Description |
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Highly self-adhesive to aramid honeycomb. Meets flammability requirements for use in aircraft interiors.
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Snap cure prepreg. Self-adhesive to honeycomb. Meets flammability requirements
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Suitable for press and bag molding. Self-adhesive to aramid honeycomb with extremely low heat release rates. (Sub 30/30 OSU)
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Snap cure prepreg. Very good adhesion and extremely low heat release rates.
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Designed for use in high temperature aerospace applications including ducting, engine components and heat shields. Tg of 310° F (155° C) |
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Exceptional char yield for carbon carbon applications and does not exhibit macro
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LR1406H* X085*
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Low fired stretch broken and spun carbon. Improved erosion resistance for solid
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* Contact Us for technical data sheets of our ablative prepreg materials