Datasheet Details
| Part number | PHG600-68-50 |
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| Manufacturer | Gurit |
| File Size | 92.63 KB |
| Description | Fiber reinforced thermosetting preimpregnated materials |
| Download | PHG600-68-50 Download (PDF) |
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Overview: www.DataSheet.co.kr PHG600-68-50 Fiber reinforced thermosetting preimpregnated materials for aircraft interior parts. Woven fabric of E-glass filament yarn Style 7781, 296 g/m2, 8H satin, preimpregnated with 53% phenolic resin PH600. Self-adhesive resin system for sandwich panel application Non-halogenated resin formulation Excellent FST behaviour Outstanding adhesion to core materials Adjustable tackiness and retarded flow during curing Long shelf and shop life PDS PHG600-68-50-1-0907 Datasheet pdf - http://www.DataSheet4U.net/ 1 www.DataSheet.co.
| Part number | PHG600-68-50 |
|---|---|
| Manufacturer | Gurit |
| File Size | 92.63 KB |
| Description | Fiber reinforced thermosetting preimpregnated materials |
| Download | PHG600-68-50 Download (PDF) |
|
|
|
PHG600-68-50 consists of a E-glass fabric Style 7781, impregnated with the phenolic resin PH600.
This resin is a halogen-free and self-adhesive phenolic system designed for wide variety of manufacturing processes, retarded flow during curing, excellent heat-release and smoke-density properties and outstanding adhesion to cores and metallic substrates.
This prepreg meets the following AIRBUS material performance specification: ABS5047-08 AIMS 05-10-002 (certification) Cured laminates fulfil the flame-retardant specifications: FAR 25.853 (self-extinguishing) The prepreg is very suitable for the manufacturing of lightweight composite sandwich structures for aircraft interior with high interlaminar shear strength and oustanding adhesion to honeycomb cores.
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