PRODUCT DATASHEET TENCATE E750 PREPREG BENEFITS/FEATURES
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1 PRODUCT TYPE 80 C (176 F) to 180 C (356 F) cure curing toughened epoxy TYPICAL APPLICATIONS Structural applications within Formula 1 SHELF LIFE PRODUCT DESCRIPTION is a toughened epoxy resin system developed for structural applications within Formula 1 and high performance automotive. The resin system allows curing from 80 C (176 F) to 180 C (356 F) and can be impregnated into a range of fibre and fabric types. TENCATE E750 PREPREG BENEFITS/FEATURES Versatile cure schedules 80 C (176 F) to 180 C (356 F) Excellent translation of fibre properties Good impact resistance Excellent retention of properties at 120 C (248 F) Controlled flow Good drape and tack 60 days outlife at 18 C (64 F) 12 months storage life at -18 C (0 F) TYPICAL NEAT RESIN PROPERTIES Density g/cm 3 (76.8 lbs/ft³) Tg (DMA) after 1 hr at 135 C (275ºF)... Onset: 148 C (298.4 F); Peak tan δ: 185 C (365 F) Out life 60 days 18 C (64 F) 000 Viscosity profiles Storage life C (0 F) Out life is the maximum time allowed at room temperature before cure. To avoid moisture condensation: Following removal from cold storage, allow the prepreg to reach room temperature before opening the polythene bag. Typically the thaw time for a full roll of material will be 4 to 6 hours. Complex viscosity (Pa.s) C/min 1 C/min 2 C/min 5 C/min Temperature ( C) Page 1 of 6
2 Ramp rate vs viscosity plot Min viscosity (Pa.s) Min Viscosity (Pa.s) Min Viscosity ( C) Ramp rate ( C/min) 0 G" loss modulus & G' storage modulus (Pa) C/min ramp Temperature ( C) Tgel = 122 C tgel = 41 mins ƞ min = 9.75 Pa.s Tƞ min = 111 C tƞ min = 35 mins G" Loss Modulus G' Storage Modulus Complex Viscosity Complex viscosity (Pa.s) CURE PROPERTIES: VISCOSITY PROFILE (40 C TO 140 C OR 4 F TO 284 F) Ramp rate [ C ( F)/min] Min viscosity (Pa.s) min viscosity C ( F) 0.5 (0.9) (203) 1 (1.8) (216) 2 (3.6) (231) 5 (9) (251) Page 2 of 6
3 TYPICAL CURE PROFILES 135 C (275 F) cure temperatures Ramp 2.0 C (3.6 F) / minute to 135 C (275 F) Dwell for 1 hour Cool 2.0 C (3.6 F) / minute to below 60 C (140 F) Followed by demould Total time: 2 hours 35 minutes INITIAL MINIMUM CURE TIMES Cure Cycle Tg Onset ( C) Tg Peak tan δ ( C) 16 hours at 80 C (176 F) hours at 0 C (212 F) hour at 135 C (275 F) minutes at 150 C (302 F) hour at 135 C (275 F) plus 2 hours at 180 C (356 F) TYPICAL LAMINATE PROPERTIES E IM CARBON T GSM 2x2 T 6K 42% R.W. CURED 1 HR AT 135 C (275 F) Property Method Test Temperature RT 120 C (248 F)) Tensile Strength (MPa) - Warp ISO Tensile Modulus (GPa) - Warp ISO Tensile Strength (MPa) - Weft ISO Tensile Modulus (GPa) - Weft ISO Poisson s Ratio ISO Compression Strength (MPa) - Warp pren Compression Modulus (GPa) - Warp pren Compression Strength (MPa) - Weft pren Compression Modulus (GPa) - Weft pren In-Plane Shear Strength (MPa) pren In-Plane Shear Modulus (GPa) pren Poisson s Ratio pren ILSS Warp (MPa) ASTM D GIC (J/m 2 ) pren Page 3 of 6
4 E IM CARBON T GSM 5HS 12K 42% R.W. CURED 1 HR AT 135 C (275 F) Property Method Test Temperature RT 120 C (248 F) Tensile Strength (MPa) - Warp ISO Tensile Modulus (GPa) - Warp ISO Tensile Strength (MPa) - Weft ISO Tensile Modulus (GPa) - Weft ISO Poisson s Ratio ISO Compression Strength (MPa) - Warp pren Compression Modulus (GPa) - Warp pren Compression Strength (MPa) - Weft pren Compression Modulus (GPa) - Weft pren In-Plane Shear Strength (MPa) pren In-Plane Shear Modulus (GPa) pren Poisson s Ratio pren ILSS Warp (MPa) ASTM D GIC (J/m 2 ) pren Page 4 of 6
5 E HM0122 -CARBON M46J 200 GSM 2X2 T 6K 42% R.W CURED 1HR AT 135 C (275 F) Property Method Test Temperature RT 120 C (248 F) Tensile Strength (MPa) - Warp ISO Tensile Modulus (GPa) - Warp ISO Tensile Strength (MPa) - Weft ISO Tensile Modulus (GPa) - Weft ISO Poisson s Ratio ISO Compression Strength (MPa) - Warp pren Compression Modulus (GPa) - Warp pren Compression Strength (MPa) - Weft pren Compression Modulus (GPa) - Weft pren In-Plane Shear Strength (MPa) pren In-Plane Shear Modulus (GPa) pren Poisson s Ratio pren ILSS Warp (MPa) ASTM D GIC (J/m 2 ) pren Page 5 of 6
6 PROCESSING Following removal from refrigerated storage, allow the prepreg to reach room temperature before opening the polythene bag, to avoid moisture condensation. Typically the thaw time for a full roll of material will be 4 to 6 hours. Cut patterns to size and lay up the laminate in line with design instructions taking care not to distort the prepreg. If necessary, the tack of the prepreg may be increased by gentle warming with hot air. The lay-up should be vacuum debulked at regular intervals using a P3 (pin pricked) release film on the prepreg surface, vacuum of 980 mbar (29 in Hg) is applied for 20 minutes. For autoclave cures, use of a non-perforated release film on the prepreg surface trimmed to within 25-30mm of prepreg edge is recommended for the cure cycle, a vacuum bag should be installed using standard techniques. EXOTHERM In certain circumstances, such as the production of thick section laminates rapid heat up rates or highly insulating masters. can undergo exothermic heating leading to rapid temperature rise and component degradation in extreme cases. Where this is likely, a cure incorporating an intermediate dwell is recommended in order to minimize the risk. Revised 02/2015 All data given is based on representative samples of the materials in question. Since the method and circumstances under which these materials are processed and tested are key to their performance, and TenCate Advanced Composites has no assurance of how its customers will use the material, the corporation cannot guarantee these properties. Page 6 of 6 Amber Drive, Langley Mill G. van der Muelenweg Butterfield Blvd. ISO 9001 Nottingham, NG16 4BE UK 7443 RE Nijverdal NL Morgan Hill, CA USA ISO Tel: +44 (0) Tel: Tel: advancedcomposites.europe@tencate.com (Europe) Registered Fax: +44 (0) Fax: Fax: info@tcac-usa.com (USA) AS 90
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