Tabulated source data are presented for wind tunnel tests conducted on scale models of the space shuttle orbiter and external tank. (Author)
Heat Transfer Tests on a 0.01-Scale Rockwell Configuration 3 Space Shuttle Orbiter and Tank (37-Ot) in the Calspan 48-Inch Hypersonic Shock Tunnel (OH12/IH21), Volume 3
1975
494 pages
Report
Keine Angabe
Englisch