johnbr

Lockheed_AH-56_Cheyenne

Specifications (AH-56A)Data from Jane's Aircraft[46] WarbirdTech AH-56A[47] General characteristics Crew: Two; one pilot, one copilot/gunner (front seat) Length: 54 ft 8 in (16.66 m) Rotor diameter: 51 ft 3 in (15.62 m) Height: 13 ft 8.5 in (4.18 m) Empty weight: 12,215 lb (5,540 kg) Loaded weight: 18,300 lb (8,300 kg) Max takeoff weight: 25,880 lb (11,740 kg) Powerplant: 1× General Electric T64-GE-16 turboshaft, 3,925 shp (2,930 kW) Rotor systems: 4 blades on main rotor, 4 blades on tail rotor, 3 blades on pusher propeller Performance Maximum speed: 212 knots (244 mph, 393 km/h) Cruise speed: 195 kn (225 mph, 362 km/h) Range: 1,063 nmi (1,225 mi, 1,971 km) Service ceiling: 20,000 ft (6,100 m) Rate of climb: 3,000 ft/min (15.23 m/s) Armament Guns: 1 × nose turret with either an M129 40 mm (1.57 in) grenade launcher or an XM196 7.62x51 mm machine gun and 1 × belly turret with an XM140 30 mm (1.18 in) cannon Hardpoints: 6 Rockets: 2.75 in (70 mm) FFA rockets Missiles: BGM-71 TOW missiles

Lockheed_AH-56_Cheyenne
johnbr, Apr 3, 2011
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  • Category:
    Helicopters
    Uploaded By:
    johnbr
    Date:
    Apr 3, 2011
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