TCR Composites
TR1110
TR1110 · Component prepreg
Matrix system
Epoxy
TR1110
Reinforcement
Carbon / glass / aramid / quartz
· Fabric broadgoods
Processing
Autoclave; OOA oven; press; filament winding / towpreg
177.00 °C
Best fit
Aerospace, industrial
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: 155.00 °C · Maximum service temperature: Not specified °C
Storage: Not specified °C · Shelf life: Not specified months · Out life: Not specified days