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HexPly® 6376 is a high performance tough matrix formulated for the fabrication of primary aircraft structures. It offers high impact resistance and damage tolerance for a wide range of high temperature applications.

Polymer Name: Epoxy Resins & Compounds

Functions: Prepreg

Technical Data Sheet

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Identification & Functionality

Composite Materials Functions

Features & Benefits

Materials Features
Product Highlights
  • Excellent toughness and damage tolerance
  • Simple straight-up cure cycle
  • Controlled matrix flow for ease of processing
  • Effective translation of fiber properties
  • Good hot/wet properties up to 150°C

Applications & Uses

Properties

Physical Form
Cured Properties
ValueUnitsTest Method / Conditions
Tensile strength at 175°C105MpaISO R527 type 1
Tensile Modulus at 175°C3.6GPaISO R527 type 1
Tensile Strain at 175°C3.1%ISO R527 type 1
Flexural strength at 175°C144MpaISO 178
Flexural Modulus at 175°C4.4GPaISO 178
Toughness G1C at 175°C432J/m2
Cured Density at 175°C1.31g/cm3

Technical Details & Test Data

Curing Conditions
  • 2 hours at 175°C and 700kN/m2 (7 bar) pressure.
  • Heat up rate 2°C to 5°C.

Components up to 30 mm thick can be cured without a dwell in the schedule provided that the heat-up rate is not more than 3°C/minute. There is no deterioration in performance after 3 times the recommended cure schedule (verified by interlaminar shear strength tests).

Storage & Handling

Shelf Life
  • Tack Life @ 23°C 10 days (still processable for up to 21 days).
  • Guaranteed Shelf Life @ -18°C 12 months (maximum, from date of manufacture)
Storage

Storage conditions.

  • HexPlyS 6376 prepregs should be stored as received in a cool dry place or in a refrigerator. After removal from refrigerator storage, prepreg should be allowed to reach room temperature before opening the polythene bag, thus preventing condensation. (A full reel in its packaging can take up to 48 hours).