Prediction of Heat Transfer Characteristics of the Carbonized Layer of Resin-Based Ablative Material Based on the Finite Element Method

Table 2

Each component’s parameters of the ablation material’s carbonized layer.

Component	Volume fraction (%)			Thermal conductivity coefficient (W·m^-1·K^-1)
	A	B	C
Carbon matrix	4.67	9.35	6.2	16
Silica fiber	0.0644	0.2323	0	0.6
Carbon fiber	0	0	0.7084	40
Microsphere	26.62	30.11	26.08	16
Poriness	68.64	60.3	67.01	0.023