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>Stagnation point envelopes of some European facilities for TPS testing and reentry trajectory of Stardust (for a European standard model of 50 mm at the exception of JP 200).</table>

International Journal of Aerospace Engineering

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Figure 7

Figure 7: 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 

Figure 7 | 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 