Wind tunnel tests were performed to determine the static aerodynamic characteristics of a model of a 60 degree swept delta wing space shuttle orbiter. Some control effectiveness tests were included. The tests were conducted in a unitary plan wind tunnel at Mach numbers of 2.50, 3.90, and 4.60. (Author)
Aerodynamic Characteristics of a 60 Degree Swept delta-Wing Space Shuttle Orbiter at Mach Numbers of 2.50, 3.90, AND 4.60
1972
116 pages
Report
No indication
English