
MATERIALS, ADHESIVES AND COATINGS
HexPly 8552 — toughened 180 °C epoxy prepreg for primary aircraft structures
Country: · Model: HexPly 8552
HexPly 8552 is a toughened epoxy prepreg that cures at 180 °C (350 °F) and is designed as a low-flow material for service up to 121 °C (250 °F). It is selected for primary aircraft structures where stiffness and damage tolerance are needed, and is supplied as tapes and fabrics of carbon, glass and other fibers.
- Matrix
- amine-cured toughened epoxy resin, cure 180 °C (350 °F), low flow
- Service temperature
- up to 121 °C (250 °F)
- Tg dry / wet
- 200 °C (392 °F) / 154 °C (309 °F)
- Neat resin
- density 1.30 g/cm³; tensile strength 121 MPa (17.5 ksi); K1C 1.475 ksi·√in
Technical specifications
| Matrix | amine-cured toughened epoxy resin, cure 180 °C (350 °F), low flow |
|---|---|
| Service temperature | up to 121 °C (250 °F) |
| Tg dry / wet | 200 °C (392 °F) / 154 °C (309 °F) |
| Neat resin | density 1.30 g/cm³; tensile strength 121 MPa (17.5 ksi); K1C 1.475 ksi·√in |
| Gel time at 177 °C | 13 min |
| Versions | 8552 (standard), 8552ATL (reduced tack for automated lay-up), 8552S |
| Reinforcement | carbon tapes and fabrics (AS4, IM7), glass, aramid, quartz, tow prepreg |
| Resin content | tapes 33–38 %, fabrics 32–42 %; volatiles ≤ 1.0–1.5 % |
| 0° tension (AS4/IM7, −55 °C) | 300 / 373 ksi |
Specifications are taken from the manufacturer’s technical documentation. Updated .
Description
The matrix is amine-cured and toughened for damage tolerance. The glass transition temperature of the neat resin is 200 °C dry and 154 °C wet, tensile strength is 121 MPa, elongation 1.7 %, and fracture toughness K1C 1.475 ksi·√in. Gelation at 177 °C takes 13 min. Carbon tapes contain 33–38 % resin, fabrics 32–42 %, and volatiles do not exceed 1.0–1.5 %. The TDS gives laminate properties from −55 to +90 °C dry and wet, including compression after impact (CAI). For 0° tension at −55 °C, tapes on AS4 and IM7 have 300 and 373 ksi. The material is supplied in rolls and stored in a freezer. Shelf life is 12 months at −18 °C, tack lasts 10 days, and outside the freezer the prepreg can sit for up to 30 days at 23 °C. Before opening, the package is warmed to room temperature, otherwise condensation will settle on the fiber.
How to choose
First determine the lay-up method. For hand lay-up the standard 8552 is taken, for automated tape laying (ATL) the 8552ATL version with reduced tack, and 8552S is another version of this matrix. If the part will operate for long periods above 121 °C, see the bismaleimide M65 and F655 up to 204 °C, and for repairing structures without an autoclave there is M20 with a cure at 130 °C.
Request a price and lead time
HexPly 8552 — toughened 180 °C epoxy prepreg for primary aircraft structures. We reply within one business day.
Or email office@usk.ua or call +38 (044) 339-50-20.
FAQ
At what temperature does HexPly 8552 cure?
At 180 °C (350 °F). Gel time at 177 °C is 13 min.
How long can the prepreg stay outside the freezer?
Up to 30 days at 23 °C, with tack lasting 10 days. Shelf life is 12 months at −18 °C.
How do 8552, 8552ATL and 8552S differ?
8552 is the standard version, 8552ATL has reduced tack for automated tape laying, and 8552S is produced as a separate variant.
What is the glass transition temperature of 8552 resin?
200 °C dry and 154 °C wet.
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