|
|
|
|
|
|||
General characteristics Crew: Crew: 2 (pilot and co-pilot gunner) Length: 58.17 ft (17.73 m) (with both rotors turning) Rotor diameter: 48 ft 0 in (14.63 m) Height: 12.7 ft (3.87 m) Disc area: 1,809.5 ft² (168.11 m²) Empty weight: 11,387 lb (5,165 kg) Loaded weight: 17,650 lb (8,000 kg) Max takeoff weight: 23,000 lb (10,433 kg) Powerplant: 2× General Electric T700-GE-701 and later upgraded to T700-GE-701C (1990-present) & T700-GE-701D (AH-64D block III) turboshafts, -701: 1,690 shp, -701C: 1,890 shp, -701D: 2,000 shp (-701: 1,260 kW, -701C: 1,490 kW, -701D: 1,490 kW) each Fuselage length: 49 ft 5 in (15.06 m) Rotor systems: 4 blade main rotor, 4 blade tail rotor in non-orthogonal alignment[46] Performance: Never exceed speed: 197 knots (227 mph, 365 km/h) Maximum speed: 158 knots (182 mph, 293 km/h) Cruise speed: 143 knots (165 mph, 265 km/h) Combat radius: 260 nmi (300 mi, 480 km) Ferry range: 1,024 nmi (1,180 mi, 1,900 km) Service ceiling: 21,000 ft (6,400 m) Rate of climb: 2,500 ft/min (12.7 m/s) Disc loading: 9.80 lb/ft² (47.90 kg/m²) Power/mass: 0.18 hp/lb (310 W/kg) Combat Mission: 167 mph Combat Range: 300 miles Combat Endurance: 2.5 hours Length: 49 ft 5 in Mission Weight: 16,600 lbs Armament: Guns: 1× 30x113 mm (1.18x4.45 in) M230 cannon, 1,200 rounds Rockets: Hydra 70 FFAR rockets Missiles: combination of AGM-114 Hellfire, AIM-92 Stinger, and AIM-9 Sidewinder Manufacturer: Airframe - Boeing (Mesa, AZ); Fire Control Radar - Northrup Grummen (Linthicum, MD); Lockheed Martin (Owego, NY); MTADS/PNVS - Lockheed Martin (Orlando, FL); Boeing (Mesa, AZ) |
|||