Cargo Compartment Liner Burn-Through Fuel Test System | ASTM ISO Testing Machine
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The Cargo Compartment Liner Burn-Through Fuel Test System is a specialized aviation fire testing platform designed to evaluate burn-through resistance, flame spread behavior, and fuel fire performance of aircraft cargo compartment liners and related materials under controlled aviation fuel fire exposure. The system integrates the FAA-approved NexGen aviation fuel burner with a dedicated seat cushion test frame and dynamic loading motion system, enabling realistic simulation of aircraft fire scenarios while accurately controlling and monitoring fuel and air parameters. Its modular design supports current regulatory testing requirements and future FAA technical upgrades.
Application
This system is suitable for aviation fuel fire testing of a wide range of aerospace materials and components, particularly those used in aircraft interiors and cargo compartments, including:
Cargo compartment liner panels
Aircraft seat cushions
Composite sandwich panels
Cabin interior panels
Ceiling and sidewall liners
Fire barrier layers
Thermal and acoustic insulation assemblies
Multi-layer composite structures
The FAA-approved NexGen burner provides standardized aviation fuel flame exposure, while the seat cushion test frame and dynamic motion system allow direct evaluation of flame behavior, burn-through risk, and material performance under realistic fire conditions.
Standards
The system supports testing in accordance with the following international aerospace fire safety standards:
BSS 7303 – Combustion performance and flame spread behavior of aerospace composite materials
AITM 2.0009 – Determination of flame spread characteristics of aerospace materials
FAR Part 25 Appendix F Part II – Aircraft cabin material combustion, flame spread, and smoke toxicity requirements
Parameters
| Item | Specification |
|---|---|
| Overall dimensions | 1500 mm (W) × 1800 mm (H) × 900 mm |
| System weight | 150 kg |
| Power requirement | 220 V, 10 A |
| Operating temperature | 10°C to 35°C |
| Fuel type | Aviation kerosene |
| Air supply | Minimum 120 PSI compressed air |
| Flame temperature capability | ≥ 2000 ± 50 ℉ |
| Heat flux output | ≥ 10.6 W/cm² |
| Temperature control bath | ≥ 2 × 0.14 m³ |
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