TCR Composites
UF3323
UF3323 · Component prepreg
Matrix system
Epoxy
UF3323
Reinforcement
Carbon / glass / aramid / quartz
· Tow; woven fabric; UD tape
Processing
Autoclave; OOA oven; press; filament winding / towpreg
138.00 °C
Best fit
Rocket motor cases, large structures
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: 125.00 °C · Maximum service temperature: Not specified °C
Storage: -18.00 °C · Shelf life: 30.00 months · Out life: 365.00 days