Hankuk Composite
3434-5E
3434-5E · Component prepreg
Matrix system
Epoxy
3434-5E
Reinforcement
Carbon / glass
· Woven / UD prepreg
Processing
Autoclave / oven
180.00 °C
Best fit
Aerospace
Construction and composition
- FAW
- Not publicly specified g/m²
- Prepreg areal weight
- Not publicly specified g/m²
- Resin content
- Not publicly specified%
- Cured ply thickness
- Not publicly specified mm
Thermal, storage and handling
Tg: 180.00 °C · Maximum service temperature: Not specified °C
Storage: Not specified °C · Shelf life: Not specified months · Out life: Not specified days