Operating characteristics of the SR5 Hypersonic Plasma Wind-Tunnel
Analysis of the radiative heat flux during the entry of the Huygens Probe in the Titan atmosphere
Multigroup model for radiating flows during atmospheric hypersonic re-entry
Prediction of nonequilibrium radiation from CO~2-N~2 shock waves
Modeling sensitivity analysis for TC3 on the orbiter aerothermal properties
Rebuilding flowfield and radiation test cases for Mars and Titan atmospheres
Development of the PHARAON platform and ONERA numerical solvers for gas radiation
Numerical simulation of non-equilibrium hypersonic CO~2 flows for Mars entry application
Computing system for solving radiative gasdynamic problems of entry and re-entry space vehicles
PARADE - a program to calculate the radiation of atmospheric re-entry in different atmospheres
Qualification of TPS components in Martian and Earth atmospheres