Experimental and Numerical Approach for the Qualification of TPS Components in Different Planetary Entry Conditions

Details Experimental and Numerical Approach for the Qualification of TPS Components in Different Planetary Entry Conditions Experimental and Numerical Approach for the Qualification of TPS Components in Different Planetary Entry Conditions

Apr 2003

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003esasp.521..177g&link_type=gif

Hot Structures and Thermal Protection Systems for Space Vehicles, Proceedings of the 4th European Workshop held 26-29 November,

Physics

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