Guangzhou Eric Wei Chemical Co., Ltd.
Guangzhou Eric Wei Chemical Co., Ltd.

Solvay FM 410-1 Adhesive

Solvay FM 410-1 Adhesive is a high-performance film adhesive in Solvay’s FM series, engineered for aerospace composite bonding. It delivers excellent toughness, thermal stability up to 180°C, low volatile content, and outstanding peel strength. Compatible with carbon fiber prepregs and metal substrates, it cures at 177°C under pressure. Widely used in structural aircraft components requiring FAA/EASA compliance and long-term durability.
  • solvay fm 410 1 adhesive_b6506f61
  • solvay fm 410 1 adhesive_b6506f61

Features Of Solvay FM 410-1 Adhesive

  1. High-performance film adhesive formulated for elevated-temperature bonding of advanced composite structures.

  2. Excellent out-life stability at ambient temperature, supporting extended handling and layup flexibility.

  3. Low volatile content and minimal outgassing, meeting stringent aerospace cleanliness requirements.

  4. Consistent rheology and tack retention during refrigerated storage (–18 °C to –25 °C).

  5. Compatible with automated tape-laying and hand-layup processes on carbon fiber and fiberglass substrates.

Typical Applications Of Solvay FM 410-1 Adhesive

  1. Aerospace primary and secondary structural bonding (e.g., wing skins, control surfaces, fairings).

  2. Thermal management assemblies in electric propulsion systems requiring high thermal cycle resistance.

  3. Defense platforms including UAV airframes and radar-absorbing structures.

  4. Racing and high-performance automotive carbon composite chassis and body components.

  5. Industrial wind turbine blade root joints and spar cap reinforcements.

Specifications Of Solvay FM 410-1 Adhesive

Chemical TypeModified epoxy-based thermoset film adhesive
Product FormPre-impregnated film (standard thickness: 0.10 mm ±0.02 mm)
AppearanceUniform amber-colored, flexible film with protective release liners
Storage Condition–25 °C; shelf life 12 months from date of manufacture
Cure Cycle (typical)180 °C / 90 min under vacuum and 0.69 MPa autoclave pressure
Glass Transition Temperature (Tg)≥175 °C (post-cure, DMA)
Primary ApplicationsStructural bonding of prepreg composites in aerospace and defense
Key FeaturesHigh toughness, low moisture uptake, excellent peel strength (>15 N/mm)


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