Radiative Heating Under Particulate-Laden Conditions During Hypersonic Planetary Entry

An important consideration while designing for hyper-sonic planetary entry is the interaction between the multitude of physical phenomena that manfist them-selves at these extreme conditions. This fact is also true for a Martian landing where in addition to thermo-chemical non-equilibriurm, vehicular predictions are impacted by radiative heating and potentially atmos-pheric dust. Previous studes have indicated that infra-red (IR) radiation emanating from CO2 and CO mole-cules constitute a significant fraction, especially in the backshell, of the total surface heat flux. In similar vein, dust particles, which can be present even under quiescent conditions, have been shown to increase the erosion rate of the heatshield. However, what remains relatively unquantified is the possible modification of the radiative environment due to the presence of dust. The present study is expected to provide the most de-tailed assessment to date of particles introducing changes to the radiative energy transfer both through the attenuation of existing shocked gas-induced radia-tion and additional emission.