The results are presented of aerodynamic heating tests conducted on a 0.0175-scale model of the space shuttle orbiter. The tests were conducted at a nominal Mach number of 8 and model angles of attack varying between 20 deg and 45 deg.
Results of heat transfer tests on a 0.0175-scale space shuttle orbiter model (56-0) in the AEDC VKF 'B' Hypersonic Wind Tunnel (OH74)
1976-02-01
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Englisch