Barrday
PH4101
PH4101 · Component prepreg
Matrix system
Phenolic
PH4101
Reinforcement
Carbon / silica / glass
· Woven prepreg
Processing
Autoclave; press; vacuum-bag / oven
— °C
Best fit
Aerospace, Defense, Propulsion
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