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>Performance envelopes (binary scaling parameter as function of velocity) of HEG, TH2, F4 and Longshot (VKI) for Earth suborbital reentry according to Kordulla et al. [<a href="/journals/ijae/2011/937629/#B34">34</a>].</table>

International Journal of Aerospace Engineering

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Figure 2

Figure 2: 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 2 | 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 