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)
Wind Tunnel Test Results for the Direction Controlled Antitank (DCAT) Missile At Mach Numbers from 0.64 to 2.50
1973
269 pages
Report
No indication
English
Ammunition, Explosives, & Pyrotechnics , Surface Launched Missiles , Antitank ammunition , Wind tunnel tests , Surface to surface missiles , Wind tunnel models , Subsonic characteristics , Transonic characteristics , Supersonic characteristics , Interference , Folding fins(Rockets) , Reaction control systems , Shoulder launched weapons , Jets , DCAT missiles , Direction controlled antitank missiles
Trigat medium-range antitank missile qualified
Online Contents | 1997
Trigat-MP: The third-generation antitank missile
Online Contents | 1999
|TRlGAT:Britain joins 3rd-generation antitank missile program
Online Contents | 1999