High-performance film adhesive specifically formulated for aerospace-grade composite bonding.
Excellent elevated-temperature resistance up to 180 °C (356 °F) after full cure.
Low volatile content and controlled tack, enabling clean handling and precise layup in automated processes.
Outstanding peel strength and fracture toughness on carbon fiber reinforced polymer (CFRP) substrates.
Compatible with standard autoclave curing cycles (e.g., 180 °C / 2 hr at 6.9 bar).
Aerospace primary and secondary structural joints in commercial and military aircraft.
Bonding of CFRP skins to honeycomb or foam core in radomes and fairings.
Repair of composite airframe components under OEM-approved procedures.
Integration of embedded sensors and metallic inserts into thermoset composite assemblies.
| Chemical Type | Modified bismaleimide (BMI) resin system |
| Product Form | Pre-impregnated unsupported film (standard thickness: 0.10 mm) |
| Appearance | Amber-colored, flexible, non-tacky film with uniform surface texture |
| Storage Condition | -18 °C (0 °F) or below; stable for 12 months when sealed and frozen |
| Processing Temperature Range | -55 °C to +60 °C (film remains handleable at room temperature for ≤72 hr) |
| Cure Cycle (Typical) | 120 °C/1 hr → 180 °C/2 hr @ 6.9 bar (autoclave) |
| Post-Cure Option | Optional 200 °C/4 hr for enhanced thermo-oxidative stability |
| Compliance | Meets ASTM D5511, BMS 8-277, and Airbus AIMS 03-01-002 requirements |
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E-mail: wangxingqiang@ericwchem.com
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Building A1, Jiete Industrial Park, Huangpu District, Guangzhou City, Guangdong Province, China