Material description

Material ID: SRK01-S1

Material type: Glass fibre reinforced aluminium sarking with polypropylene polymer backing.

Polymer: Polypropylene (92%)

Additives (fire retardants, fillers or traces of inorganic elements): Chlorine (3%), Calcium (3%), Titanium (2%), Aluminium (1%), traces of other elements (<1%)

Core thickness: 0.27mm

 

Table 1. Estimated mass concentration of compounds.
CompoundMass Concentration (%)
Polypropylene (PP)92
Chlorine (Cl)3
Calcium (Ca)3
Titanium (Ti)2
Aluminium (Al)1
Traces of iron (Fe)<1
Traces of bromine (Br)<1
Traces of sulfur (S)<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
Polypropylene (PP)
...
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.
ElementMass Concentration (%)
Cl3
Ca3
Ti2
Al1
Fe<1
Br<1
S<1
Si<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.
ConditionFraction of mass residue at 800°C
Non-oxidative (nitrogen)0.03
Oxidative (air)0.03
Table 4. Temperature and amplitude of main peaks in non-oxidative conditions.
Peak IDTemperature peak (°C)Amplitude of peak (°C-1)
Peak 14672.128 x 10-2
Table 5. Temperature and amplitude of main peaks in oxidative conditions.
Peak IDTemperature peak (°C)Amplitude of peak (°C-1)
Peak 12674.74 x 10-3
Peak 23628.15 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.
TrialΔHc [kJ g-1]
Trial 142.44
Trial 241.39
Trial 342.54
Average42.12
Std dev0.64

D. Ignition parameters

Table 8. Summary of ignition parameters for sample.
Critical heat flux for ignitionIgnition temperatureTotal heat transfer coefficient of lossesApparent thermal inertia
q̇″cr [kW m−2]Tig [°C]hr [W m-2 K-1]kρc [kW2 m-4 K-2 s]
1334436.100.127
...
Figure 6. Time-to-ignition vs incident radiant heat flux for samples.

E. Burning behaviour

Table 9. Summary of key burning behaviour metrics.
Heat fluxTestTime to ignitionFraction of mass residuePeak heat release rateTotal energy released
q̇″inc [kW m-2] tig [s]mres [-]q̇″p [kW m-2]Qt [MJ m-2]
35 kW m-2
Test 1500.02131.733.22
Test 2450.06118.103.12
Avg480.04124.913.17
50 kW m-2
Test 1250.03151.693.26
Test 2200.02146.173.20
Avg220.02148.933.23
60 kW m-2
Test 1----
Test 2----
Avg----
80 kW m-2
Test 120.08210.683.18
Test 210.11217.903.25
Avg1.500.09214.293.21
...
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.
TestΔHc [kJ g-1]
35 kW m-2 (Test 1)38.76
35 kW m-2 (Test 2)38.44
50 kW m-2 (Test 1)38.34
50 kW m-2 (Test 2)37.89
60 kW m-2 (Test 1)-
60 kW m-2 (Test 2)-
80 kW m-2 (Test 1)40.28
80 kW m-2 (Test 2)42.24
Average39.32
Std dev1.64

F. Flame Spread

Table 11. Minimum heat flux for flame spread rate and minimum flame spread rate for sample.
Orientationq̇″min.spread [kW m-2]Vf.min [mm s-1]
Horizontal9.500.20
Vertical90.70
...
Figure 9. Lateral flame spread rate versus heat flux.
...
Figure 10. Vertical flame spread rate versus heat flux.
Table 12. Flame spread parameter results for sample.
OrientationTrial(kρcpΦh2)12 [m32 s12 kW-1]Φ [kW2 m-3]
Horizontal1100-
Horizontal2100-
Vertical1100-
Vertical2100-
Additional information:

1. Excessive shrinkage away from the heat source and pilot ignitor prevented the establishment of a uniform flame front 2. Melting and dripping of material during test forming flaming droplets 3. A wire mesh was placed in front of the sample to prevent curling of the material.