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.
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
1968
45 pages
Report
Keine Angabe
Englisch
Aircraft , Aerodynamics , Guns , Helicopters , Flight testing , Aerial gunnery , Firing tests(Ordnance) , Aircraft guns , Grenades , Projectors(Ordnance) , Performance(Engineering) , Aerodynamic characteristics , Stability , Control , Pilots , Visibility , Air-to-surface , Army aircraft , Close support , Aircraft turrets , Tactical air support , Hueycobra , H-1 aircraft , M-129 grenade launchers(40-mm) , M-28 turrets