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

Table 7

Stagnation point radiative heating rate comparisons for FIRE II.

𝑉𝑒 (km/s)	𝛾𝑒^∘	𝑚/(𝐶𝑑)(𝑆) (kg/m^2)	𝑉∞ (km/s)	𝑞̇conv W/cm^2	𝑞̇rad W/cm^2	𝑞̇tot W/cm^2
11.37	−8.5	40	9.25	325	10	335
12.50	−10.0	40	10.47	510	108	618
14.26	−10.0	40	11.86	730	360	1090