Accession Number:

AD0836901

Title:

ENGINEERING FLIGHT TEST OF THE AH-1G (HUEYCOBRA) HELICOPTER EQUIPPED WITH THE XM-28 CHIN TURRET WITH TWIN XM-129, 40MM GRENADE LAUNCHERS, PHASE B, PART 4

Descriptive Note:

Final rept. 10 Jan-29 Feb 1968

Corporate Author:

ARMY AVIATION SYSTEMS TEST ACTIVITY EDWARDS AFB CA

Personal Author(s):

Report Date:

1968-03-01

Pagination or Media Count:

46.0

Abstract:

Firing tests were conducted to determine the effects on the stability and control characteristics of the AH-1G helicopter caused by firing the twin XM-129, 40mm grenade launchers in the XM-28 chin turret.

Subject Categories:

  • Aerodynamics
  • Helicopters
  • Guns

Distribution Statement:

APPROVED FOR PUBLIC RELEASE