A wind tunnel test of the space shuttle orbiter configuration 040A was run in a 20 in. supersonic wind tunnel. Basic aerodynamic data for this vehicle were determined at Mach 2.0, 2.4, 3.0 and 4.0. (Author)
Space Shuttle Supersonic Aerodynamic Characteristics of the Msc 040A Orbiter (M Equals 2.0 to 4.0)
1972
314 pages
Report
No indication
English