ACP01

Material description

Material ID: ACP01

Material type: Aluminium composite panel with a predominantly inorganic core.

Polymer: Ethylene-vinyl acetate (7%)

Additives (fire retardants, fillers or traces of inorganic elements): Calcium Carbonate (51%), Alumina Trihydrate (20%), Magnesium Hydroxide (13%), Silicon Oxide (8%), Sulfur (1%), traces of other elements (<1%)

Core thickness: 2.81mm

Thickness of single metal skin: 0.82mm

Table 1. Estimated mass concentration of compounds.

Compound	Mass Concentration (%)
Ethylene-vinyl acetate (EVA)	7
Calcium Carbonate (CaCO3)	51
Alumina Trihydrate (Al(OH)3)	20
Magnesium Hydroxide (Mg(OH)2)	13
Silicon Oxide (SiO2)	8
Sulfur (S)	1
Traces of sodium (Na)	<1
Traces of potassium (K)	<1
Traces of iron (Fe)	<1
Traces of scandium (Sc)	<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)
Calcium Carbonate (CaCO3)
Alumina Trihydrate (Al(OH)3)
Magnesium Hydroxide (Mg(OH)2)

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 (%)
Ca	38
Al	8
Mg	6
Si	5
S	1
Fe	<1
K	<1
Na	<1
Sc	<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)	0.73
Oxidative (air)	0.72

Table 4. Temperature and amplitude of main peaks in non-oxidative conditions.

Peak ID	Temperature peak (°C)	Amplitude of peak (°C^-1)
Peak 1	290	1.55 x 10^-3
Peak 2	324	2.15 x 10^-3
Peak 3	744	1.43 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	289	1.8 x 10^-3
Peak 2	316	1.7 x 10^-3
Peak 3	742	1.32 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	ΔH_c [kJ g^-1]
Trial 1	2.60
Trial 2	2.23
Trial 3	2.28
Average	2.37
Std dev	0.20

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]	T_ig [°C]	h_r [W m^-2 K^-1]	kρc [kW² m^-4 K^-2 s]
32.70	539	56.70	1.348

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]		t_ig [s]	m_res [-]	q̇″_p [kW m^-2]	Q_t [MJ m^-2]
35 kW m^-2
	Test 1	229	0.74	53.87	7.19
	Test 2	275	0.80	46.42	18.49
	Avg	252	0.77	50.15	12.84
50 kW m^-2
	Test 1	127	0.79	120.32	10.61
	Test 2	143	0.78	98.96	11.09
	Avg	135	0.79	109.64	10.85
60 kW m^-2
	Test 1	106	0.79	110.46	11.59
	Test 2	105	0.80	129.48	10.68
	Avg	106	0.79	119.97	11.14
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.

Table 10. Effective Heat of Combustion individual results for sample.

Test	ΔH_c [kJ g^-1]
35 kW m^-2 (Test 1)	5.36
35 kW m^-2 (Test 2)	16.40
50 kW m^-2 (Test 1)	9.31
50 kW m^-2 (Test 2)	9.40
60 kW m^-2 (Test 1)	9.97
60 kW m^-2 (Test 2)	8.83
80 kW m^-2 (Test 1)	-
80 kW m^-2 (Test 2)	-
Average	9.88
Std dev	3.59

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]	V_f.min [mm s^-1]
Horizontal	100	-
Vertical	100	-

Table 12. Flame spread parameter results for sample.

Orientation	Trial	(^kρc_p⁄_Φh²)^¹⁄₂ [m^³⁄₂ s^¹⁄₂ kW^-1]	Φ [kW² m^-3]
Horizontal	1	100	-
Horizontal	2	100	-
Vertical	1	100	-
Vertical	2	100	-

Additional information:

Localised ignition occurs but there is no spread of flame on the surface below the critical heat flux for ignition.