Toray Advanced Composites
TC1810
TC1810 · Component prepreg
Matrix system
Preceramic polysiloxane
TC1810
Reinforcement
Carbon / glass / aramid / quartz / specialty
· UD tape / woven / fabric prepreg
Processing
Prepreg; Autoclave; Press
— °C
Best fit
Aerospace, Space, Defence, 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: Not specified °C · Maximum service temperature: Not specified °C
Storage: Not specified °C · Shelf life: Not specified months · Out life: Not specified days