The paper focuses on the experiments performed in the European high-enthalp
y facilities during the manned space flight hypersonic ground testing techn
ology programme. Emphasis is placed on simple configuration testing enablin
g validation of the physical modelling within non-equilibrium Navier-Stokes
codes. The high-enthalpy facilities used are the ONERA hot-shot F4 and the
DLR Stalker tube HEG. The simple configurations are the nozzle, the Electr
e blunt cone, the hyperboloid flare, and the 70 degrees blunt cone. in addi
tion to these axisymmetric configurations, the Halis/Orbiter configuration
was extensively tested and numerically computed to validate the ground-to-f
light extrapolation methodology. Real-gas effects on aerodynamic forces and
in particular on pitching moment for the Halls have been reproduced in the
F4 and compared with flight. The paper concludes with a series of recommen
dations for additional improvements in nozzle calibrations using nonintrusi
ve methods, and for an increased use of computational fluid dynamics for th
e design of experiments, the definition of the test environment, the interp
retation of the results and for extrapolation to flight.