Renegade Materials
RM-2008
RM-2008 · Component prepreg
Matrix system
Modified epoxy
RM-2008
Reinforcement
Carbon / S2-glass / E-glass / Astroquartz / aramid / other
· Fabric prepreg / UD tape
Processing
Autoclave
121.00 °C
Best fit
Aerospace, Space, Defence
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