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.
Descriptors:
Subject Categories:
- Aerodynamics
- Helicopters
- Guns