Stable fibre/epoxy structures with excellent physical mechanical properties for aerospace and industrial applications.
| Fabric areal weight |
150, 200, 300, 400, 600, 800, 1000, 1600gsm and others |
| Resin content ( w% ) |
32, 38 and others |
| Glass transition temperature |
110 and others |
| Fabric construction |
UD fabrics, bi-axial woven and warp-knitted multiaxial fabrics |
| Shelf life |
1 month @ RT, min, 6months @ -18℃ |
AEROSPACE
Carbon fiber prepregs are widely used in aircraft construction as an alternative to heavy-weight materials in primary and secondary structure applications such as flaps,ailerons,spoilers, elevators, hatches, floors and interior panels.