ACP02
Material description
Material ID: ACP02
Material type: Aluminium composite panel with a core consisting of ethylene-vinyl acetate (EVA) and a fire retardant.
Polymer: Ethylene-vinyl acetate (28%)
Additives (fire retardants, fillers or traces of inorganic elements): Alumina Trihydrate (72%), Magnesium (1%), traces of other elements (<1%)
Core thickness: 2.9mm
Thickness of single metal skin: 0.5mm

| Compound | Mass Concentration (%) |
|---|---|
| Ethylene-vinyl acetate (EVA) | 28 |
| Alumina Trihydrate (Al(OH)3) | 72 |
| Magnesium (Mg) | 1 |
| Traces of sodium (Na) | <1 |
| Traces of silicon (Si) | <1 |
A. Material composition identification
A.1 Attenuated total reflection – Fourier transform infrared spectroscopy (ATR-FTIR)
Table 2. FTIR compound identification.| Identified Compounds |
|---|
| Ethylene-vinyl acetate (EVA) |
| Alumina Trihydrate (Al(OH)3) |

Figure 1 . FTIR spectra: Absorbance percentage versus wavenumber from the sample.

Figure 2. FTIR spectra: Absorbance percentage versus wavenumber from the sample and the identified compounds.
A.2 Energy Dispersive X-Ray Fluorescence (EDXRF)
Table 2. Inorganic elements and their mass concentration identified with EDXRF.
| Element | Mass Concentration (%) |
|---|---|
| Al | 22 |
| Mg | <1 |
| Si | <1 |
| Ca | <1 |

Figure 3. EDXRF spectra. Counts vs energy. Identified elements are shown as vertical lines.
B. Thermogravimetric analysis
Table 3. Mass fraction of residue after thermal decomposition.
| Condition | Fraction of mass residue at 800°C |
|---|---|
| Non-oxidative (nitrogen) | 0.47 |
| Oxidative (air) | 0.46 |
Table 4. Temperature and amplitude of main peaks in non-oxidative conditions.
| Peak ID | Temperature peak (°C) | Amplitude of peak (°C-1) |
|---|---|---|
| Peak 1 | 246 | 1.06 x 10-3 |
| Peak 2 | 315 | 4.14 x 10-3 |
| Peak 3 | 483 | 7.24 x 10-3 |
Table 5. Temperature and amplitude of main peaks in oxidative conditions.
| Peak ID | Temperature peak (°C) | Amplitude of peak (°C-1) |
|---|---|---|
| Peak 1 | 247 | 1.23 x 10-3 |
| Peak 2 | 316 | 5.55 x 10-3 |
| Peak 3 | 384 | 1.8 x 10-3 |
| Peak 4 | 511 | 1.2 x 10-3 |

Figure 4. Normalised mass (solid line) and derivative of the normalised mass (dashed line) in 150 ml min-1 of nitrogen and a heating rate of 20°C min-1.

Figure 5. Normalised mass (solid line) and derivative of the normalised mass (dashed line) in 150 ml min-1 of air and a heating rate of 20°C min-1 .
C. Gross Heat of Combustion
Table 7. Gross Heat of Combustion individual results for sample.| Trial | ΔHc [kJ g-1] |
|---|---|
| Trial 1 | 12.99 |
| Trial 2 | 12.94 |
| Trial 3 | 13.29 |
| Average | 13.07 |
| Std dev | 0.19 |
D. Ignition parameters
Table 8. Summary of ignition parameters for sample.| Critical heat flux for ignition | Ignition temperature | Total heat transfer coefficient of losses | Apparent thermal inertia |
|---|---|---|---|
| q̇″cr [kW m−2] | Tig [°C] | hr [W m-2 K-1] | kρc [kW2 m-4 K-2 s] |
| 15.60 | 378 | 39.20 | 1.643 |

Figure 6. Time-to-ignition vs incident radiant heat flux for samples.
E. Burning behaviour
Table 9. Summary of key burning behaviour metrics.
| Heat flux | Test | Time to ignition | Fraction of mass residue | Peak heat release rate | Total energy released |
|---|---|---|---|---|---|
| q̇″inc [kW m-2] | tig [s] | mres [-] | q̇″p [kW m-2] | Qt [MJ m-2] | |
| 35 kW m-2 | |||||
| Test 1 | 138 | 0.73 | 119.95 | 44 | |
| Test 2 | 150 | 0.45 | 113.55 | 25.35 | |
| Avg | 144 | 0.59 | 116.75 | 34.68 | |
| 50 kW m-2 | |||||
| Test 1 | 75 | 0.46 | 145.20 | 58.01 | |
| Test 2 | 75 | 0.43 | 145.40 | 55.78 | |
| Avg | 75 | 0.45 | 145.30 | 56.90 | |
| 60 kW m-2 | |||||
| Test 1 | 66 | 0.42 | 184.46 | 57.30 | |
| Test 2 | 62 | 0.41 | 202.49 | 63.95 | |
| Avg | 64 | 0.41 | 193.48 | 60.63 | |
| 80 kW m-2 | |||||
| Test 1 | - | - | - | - | |
| Test 2 | - | - | - | - | |
| Avg | - | - | - | - |

Figure 7. Normalised mass loss over time for samples tested with 35, 50, 60 and 80 kW m-2.

Figure 8. Heat release rate per unit area over time for samples tested with 35, 50, 60 and 80 kW m-2.
| Test | ΔHc [kJ g-1] |
|---|---|
| 35 kW m-2 (Test 1) | 34.45 |
| 35 kW m-2 (Test 2) | 9.45 |
| 50 kW m-2 (Test 1) | 21.31 |
| 50 kW m-2 (Test 2) | 20.59 |
| 60 kW m-2 (Test 1) | 20.69 |
| 60 kW m-2 (Test 2) | 23.63 |
| 80 kW m-2 (Test 1) | - |
| 80 kW m-2 (Test 2) | - |
| Average | 21.68 |
| Std dev | 7.98 |
F. Flame Spread
Table 11. Minimum heat flux for flame spread rate and minimum flame spread rate for sample.| Orientation | q̇″min.spread [kW m-2] | Vf.min [mm s-1] |
|---|---|---|
| Horizontal | 100 | - |
| Vertical | 100 | - |
| Orientation | Trial | (kρcp⁄Φh2)1⁄2 [m3⁄2 s1⁄2 kW-1] | Φ [kW2 m-3] |
|---|---|---|---|
| Horizontal | 1 | 100 | - |
| Horizontal | 2 | 100 | - |
| Vertical | 1 | 100 | - |
| Vertical | 2 | 100 | - |
Sample ignites but fails to establish a uniform flame front and does not spread below the critical heat flux for ignition.