Pre Preg

HOT MELT PROCESS - OWN FORMULATION

Epoxy120 and 180°C - Cyanate Ester

- Structural matrix qualified for aerospace

- Epoxy Matrix which replace phenolic Matrix for interior cabin: FAR 25 and ADB 031

- Low Permitivity < 2,92 for space and radome

- Tooling pre preg: low initial cure from 50°C

CTMI PRE PREG img1
CTMI PRE PREG img2
CTMI PRE PREG img3
CTMI PRE PREG im41
CLASS REF DESCRIPTION
120°C 1201 C Epoxy 120°C - Conductor
1212-A Standard
1213 Standard
T.A. 1260 M TG 44° C
CLASS REF DESCRIPTION
120°C  1808 NA  Structural aeronautics - tablecloth version
1808S C1 Epoxy 120°C - Electrically conductive
1808S Standard industrie - Self-extinguishing < 300 secondes
1808S A4 Standard industrie - Cooking time 30 minutes @120°C
1814 Standard industrie - decorative transparent without white dots
1846 Structural aeronautics - TG steamy heat > 120°C
1115 Structural industrie - M2 F1 Self-extinguishing < 120 secondes
1115 A4 Structural industrie - Cooking time 30 minutes @ 120°C M2 F1 - Self-extinguishing < 120 secondes
1120 Structural industrie - M1 F1 V0 Self-extinguishing < 60 secondes
LILAS Aeronautics - Far 25 - AIRBUS - ABD 0031 Self-extinguishing < 15 secondes
180°C 1713 BS Standard - structural
1713 E Grid version
1721 Structural – dielectric value 3
1721 SM Structural – standard dielectric constant
1723 Structural – Modified improved toughness
50 and/or 120°C 1850 Tooling cuisson 50°C PC 2h à 120°C or PC 2h à 180°C
230°C 1731 NS Structural – TG 300°C with PC 2h à 250°C
1730-21 Structural – TG 300°C – dielectric value 3
CLASS REF DESCRIPTION
180°C 1950 Pure - PC 250°C - TG > 300°C - Self-extinguishing
1951 Pure Low flow - PC 250°C - TG > 300°C - Self-extinguishing
135 or 180°C 1952 Modified improved toughness PC 250°C TG 300°C
1954 Improved dielectric properties - PC 250°C TG 300°C
CLASS REF DESCRIPTION
120°C 1120-C Structural industrie - M1 F1 V0 Self-extinguishing < 60 secondes
180°C 4021 RTM
CLASS REF DESCRIPTION
100°C FIX3 Epoxy for preforms
180°C FIX180 Epoxy for preforms