(Contact Us for further information on the materials listed below or any other Barrday products)
| Product | Description | 
| 
 | High temperature semi-crystalline polymer with low moisture absorption and Tg of 200° F (95° C) 
 | 
| 
 | 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) 
 | 
| 
 
 | Same benefits as PEEK with a wider and lower temperature processing window. Tg of 303° F (151° C) | 
| 
 | 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) 
 | 
| 
 | High temperature tough amorphous polymer with excellent FST properties. | 
| Semi-crystalline polymer with good combination of strength, toughness, chemical and solvent resistance. 
 | 
| Product | Description | 
| Toughened epoxy prepreg system suitable for autoclave, press or bag molding operations. Fire retardant per FAR 25.853. Tg of 300° F (150° C) 
 | |
| 
 | 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. 
 | 
| 
 | 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. 
 | 
| 
 | High temperature curing, fire retardant epoxy per FAR 25.853. Excellent combination of toughness and high Tg of 300°F (150° C) 
 | 
| Product | Description | 
| 
 | Highly self-adhesive to aramid honeycomb. Meets flammability requirements for use in aircraft interiors. 
 | 
| 
 | Snap cure prepreg. Self-adhesive to honeycomb. Meets flammability requirements 
 | 
| 
 | Suitable for press and bag molding. Self-adhesive to aramid honeycomb with extremely low heat release rates. (Sub 30/30 OSU) 
 | 
| 
 | Snap cure prepreg. Very good adhesion and extremely low heat release rates. 
 | 
| 
 
 | Designed for use in high temperature aerospace applications including ducting, engine components and heat shields. Tg of 310° F (155° C) | 
| 
 | Exceptional char yield for carbon carbon applications and does not exhibit macro 
 | 
| LR1406®H* X085®* 
 | Low fired stretch broken and spun carbon. Improved erosion resistance for solid | 
| LR1504* | Silica fabric coated with silica-filled PSR133 resin 
 | 
| LR1750* | Graphite fabric coated with carbon-filled PSR133 resin 
 | 
* Contact Us for technical data sheets of our ablative prepreg materials