TCR Composites
TR1111
TR1111 · Component prepreg
Matrix system
Epoxy
TR1111
Reinforcement
Carbon / glass / aramid / quartz
· Tow; woven fabric
Processing
Autoclave; OOA oven; press; filament winding / towpreg
121.00 °C
Best fit
COPV, rocket motor cases, sports
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: 111.00 °C · Maximum service temperature: Not specified °C
Storage: Not specified °C · Shelf life: Not specified months · Out life: 90.00 days