An experimental investigation was conducted on a model of a wing control version of the Sparrow III type missile to determine the static aerodynamic characteristics over an angle of attack range from 0 deg to 40 deg for Mach numbers from 1.50 to 4.60.
Supersonic Aerodynamic Characteristics of a Sparrow 3 Type Missile Model with Wing Controls and Comparison with Existing Tail-Control Results
1977
84 pages
Report
No indication
English