Renegade Materials
RM-2005
RM-2005 · Component prepreg
Matrix system
Toughened epoxy
RM-2005
Reinforcement
Carbon / S2-glass / E-glass / Astroquartz / aramid / other
· Fabric prepreg / UD tape
Processing
Autoclave
177.00 °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: 185.00 °C · Maximum service temperature: Not specified °C
Storage: Not specified °C · Shelf life: Not specified months · Out life: Not specified days