Accession Number:

AD0784121

Title:

Wind Tunnel Test Results for the Direction Controlled Antitank (DCAT) Missile At Mach Numbers from 0.64 to 2.50.

Descriptive Note:

Technical rept.,

Corporate Author:

CHRYSLER CORP NEW ORLEANS LA SPACE DIV

Personal Author(s):

Report Date:

1973-10-12

Pagination or Media Count:

269.0

Abstract:

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

Subject Categories:

  • Guided Missile Dynamics, Configurations and Control Surfaces
  • Surface-Launched Guided Missiles
  • Ammunition and Explosives

Distribution Statement:

APPROVED FOR PUBLIC RELEASE