Review Article

Survey of European and Major ISC Facilities for Supporting Mars and Sample Return Mission Aerothermodynamics and Tests Required for Thermal Protection System and Dynamic Stability

Table 5

Maximum heat fluxes for EVD mission [6].

TrajectoryConvective flux kW/m2Radiative flux kW/m2Total flux kW/m2Total heat load MJ/m2

E111500750018800106.9
E2157001810033800178.3
E39350455013900243.2
E4700019008900154.6