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 class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td align="left">Trajectory</td><td align="center">Stagnation pressure at max. heat flux (Pa)</td><td align="center">Maximum stagnation pressure (Pa)</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td align="left">E1</td><td align="center">70396</td><td align="center">131500</td></tr><tr><td align="left">E2</td><td align="center">138037</td><td align="center">277339</td></tr><tr><td align="left">E3</td><td align="center">48534</td><td align="center">80300</td></tr><tr><td align="left">E4</td><td align="center">26687</td><td align="center">41180</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Maximum stagnation pressures for an EVD mission [<a href="/journals/ijae/2011/937629/#B6">6</a>]. 

International Journal of Aerospace Engineering

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Table 4

Table 4: 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 4 | 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 