]>High-Fidelity Aerothermal Engineering Analysis for Planetary Probes Using DOTNET Framework and OLAP Cubes Database : Table 11
Table 11: Material and thermal properties of carbon and silicon-based ablators.

MaterialMaterial typeDensity ( 𝜌 ) (kg/ m 3 )Thermal conductivity ( 𝜅 ) (watt/m- k )Specific heat ( 𝐶 𝑝 ) (J/kg- k )

ATJCarbon-based1729.21179.69711.76
Avcoat-5026-39Silicon based512.625.001110.0
RCCReusable CC1650.2120.01312.0