Aerospace

The 2510 Prepreg system is specifically formulated for out-of-autoclave (OOA) processing of aerospace primary structures. This Prepreg system has balanced mechanical properties and flexible curing capabilities.

Data provided herein was produced at the nominal cure temperature of 270°F.

2511 is a semi-toughened epoxy Prepreg system that was specifically formulated for better processing when compared with 2510. Our 2511 resin system can provide good structural properties and very low void content when processed in a variety of methods, including vacuum bag only (VBO) and press molding.

Data provided herein was produced at the nominal cure temperature of 270°F.

3900 series Prepregs are highly-toughened 350°F (177°C) cure systems. Our 3900 series Prepregs are available in a variety of configurations, including unidirectional tape for manual or automated tape laying applications, slit-tape-tow for automated fiber placement applications, and plain-weave carbon and glass fabrics.

Used extensively in commercial aircraft primary structure.

Toray’s next-generation 3960 Prepreg system demonstrates the next leap in performance of aerospace materials.

Pairing the 3960 resin system with T1100-series IM+ carbon fiber provides an optimal ratio of strength to modulus properties. Our 3960 series Prepregs are highly-toughened 350°F (177°C) cure systems that are available in a variety of configurations.

Used in aerospace applications where material performance is the highest priority.