Phenolic FRP Fire-Resistant Composite System
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
| Parameter | Value |
|---|---|
| Cure Schedule | 80-120°C / 1-4h (oven or IR) |
| Ambient Pot Life | 4-8 hours |
| FAR 25.853 Compliance | Yes |
| 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
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.
Direct Contact
💬WhatsApp +86 156 3910 0440Telegram +86 156 3910 0440✉️[email protected]Reply within 24 hours
Related Products
Phenolic Resole Resin (Liquid, pH 7-8)
CAS 9003-35-4
Highest FST performance in thermoset category (LOI >65%)
Phenolic Pultrusion Resin (Fire-Resistant FRP Profile)
CAS 9003-35-4
UL94 V-0, EN 45545 HL3 fire performance — unachievable with polyester
Modified Toughened Phenolic Resin (Epoxy or Rubber-Modified)
CAS 9003-35-4
40-80% improvement in impact strength over unmodified phenolic