Phenolic FRP Fire-Resistant Composite System

CAS 9003-35-4In StockSample available

Key Features

  • LOI >55% and Ds,max <100 for aircraft and railway FST compliance
  • Ambient temperature processing — no autoclave required
  • Compatible with hand lay-up, spray-up, and vacuum infusion
  • Latent acid catalyst provides 4-8h ambient pot life
  • HCN generation <30 ppm — meets EN 45545 toxic gas requirements

Phenolic FRP Fire-Resistant Composite System is an optimized phenolic resole resin system designed for manufacturing fire-resistant glass fiber reinforced composite panels, cladding, and structural components meeting the most stringent FST (fire, smoke, toxicity) requirements in enclosed public spaces. The system is specifically formulated for hand lay-up, wet winding, spray-up, and vacuum infusion processes, enabling fabrication of complex shapes not possible with press-molded phenolic compounds.

The composite system uses a medium-viscosity liquid resole (300-1,500 mPa·s at 25°C) with latent acid accelerator providing controlled ambient pot life (4-8 hours) and rapid cure at 80-120°C (oven or infrared). The cured glass/phenolic composite achieves LOI >55%, Ds,max (smoke density) <100 (ASTM E662), CO generation <1,000 ppm, and HCN <30 ppm under ASTM E1678 toxic gas test — performance required for aircraft interior FAR 25.853 and European railway EN 45545-2 HL3 compliance.

The system is designed to be processed in standard composite manufacturing facilities with ventilation upgrades for free phenol and formaldehyde handling. Ambient temperature lay-up with hot oven cure at 80-100°C eliminates the need for autoclave or press equipment, reducing capital investment for fire-resistant composite manufacturers. Applications span aircraft galleys, overhead bins, partition walls, train saloon panels, ship bulkheads, tunnel lining panels, and offshore topsides enclosed space structural panels.

Specifications

ParameterValue
Cure Schedule80-120°C / 1-4h (oven or IR)
Ambient Pot Life4-8 hours
FAR 25.853 ComplianceYes
Resin Viscosity (25°C)300-1,500 mPa·s
HCN Generation (ASTM E1678)<30 ppm
LOI (glass/phenolic composite)>55%
Smoke Density (ASTM E662, Ds,max)<100

Applications

Aircraft interior panels (galleys, overhead bins, partitions)Railway passenger saloon cladding and structural panelsShip interior bulkhead and ceiling panels (IMO FTP)Tunnel lining and underground structural panelsOffshore enclosed-space structural cladding panels

FAQ

FAR 25.853 aircraft interior material qualification requires: (1) Vertical Burn Test (FAR 25.853(a) App. F Part I): specimen 76×305mm, 12-second flame application, pass criteria: burn length ≤152mm, flame time after removal ≤15 seconds, drip flame time ≤5 seconds; (2) Heat Release Rate (FAR 25.853(d) App. F Part IV): OSU calorimeter test at 35 kW/m² heat flux, pass criteria: peak heat release ≤65 kW/m², total heat release in 2 minutes ≤65 kW·min/m²; (3) Smoke Density (FAR 25.853(d) App. F Part V): NBS smoke chamber, pass criteria: Ds,max ≤200 at both flaming and non-flaming modes. For Class A cabin materials (interior panels, overhead bins), all three tests are required. Phenolic glass composites typically pass all three with significant margin. FAR 25.853 compliance requires testing by an FAA/EASA-accepted laboratory and inclusion in the material's approval documentation.

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