Accession Number:

AD0488791

Title:

ENGINEERING FLIGHT TEST OF UH-1B HELICOPTER EQUIPPED WITH XM-16 ARMAMENT SUBSYSTEM AND ENGINEERING FLIGHT TEST OF UH-1B HELICOPTER EQUIPPED WITH XM-21 ARMAMENT SUBSYSTEM

Descriptive Note:

Final test rept. 19 Jul-2 Sep 1965

Corporate Author:

ARMY AVIATION SYSTEMS TEST ACTIVITY EDWARDS AFB CA

Personal Author(s):

Report Date:

1966-06-01

Pagination or Media Count:

155.0

Abstract:

Engineering flight tests of the UH-1B helicopter equipped with the XM-16 and XM-21 armament subsystems were conducted. The overall objective was to determine the effect of the installation of the subsystems on the UH-1B. Specific objectives were to determine the existence of any safety-of-flight conditions by evaluation of equantitative stability and control and vibration data and to determine any performance losses.

Subject Categories:

  • Helicopters
  • Guns

Distribution Statement:

APPROVED FOR PUBLIC RELEASE