Research Article

High-Fidelity Aerothermal Engineering Analysis for Planetary Probes Using DOTNET Framework and OLAP Cubes Database

Table 11

Material and thermal properties of carbon and silicon-based ablators.

MaterialMaterial typeDensity ( ) (kg/ )Thermal conductivity ( ) (watt/m- )Specific heat ( ) (J/kg- )

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