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

Table 1

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

Component	Volume fraction (%)			Thermal conductivity coefficient (W·m^-1·K^-1)
	A	B	C
Phenolic matrix	21.57	43.16	28.61	0.2
Silica fiber	0.06435	0.2323	0	0.6
Carbon fiber	0	0	0.7084	40
Microsphere	33.74	38.16	33.05	0.2
Poriness	44.63	18.45	37.63	0.023