Wind Tunnel Test Results for the Direction Controlled Antitank (DCAT) Missile At Mach Numbers from 0.64 to 2.50.
CHRYSLER CORP NEW ORLEANS LA SPACE DIV
Pagination or Media Count:
Wind tunnel test results are presented to show aerodynamic characteristics over the Mach number range of 0.64 to 2.50 of the DCAT missile. Data are presented showing the interference created by the rear mounted reaction control system. Two candidate fins were installed on the model during tests a flat folding fin and a curved wrap around fin. Author
- Guided Missile Dynamics, Configurations and Control Surfaces
- Surface-Launched Guided Missiles
- Ammunition and Explosives