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
||UD fabrics, bi-axial woven and warp-knitted multiaxial fabrics
||1 month @ RT, min, 6months @ -18℃
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.