UH-1 (Specifications)

Specifications of the UH-1


*General characteristics:
Crew: 1-4
Capacity: 3,880 lb including 14 troops, or 6 stretchers, or equivalent cargo
Length: 57 ft 1 in with rotors (17.4 m)
Fuselage width: 8 ft 7 in (2.6 m))
Rotor diameter: 48 ft 0 in (14.6 m)
Height: 14 ft 5 in (4.4 m)
Empty weight: 5,215 lb (2,365 kg)
Loaded weight: 9,040 lb (4,100 kg)
Max takeoff weight: 9,500 lb (4,310 kg)
Fuel capacity: 1,400 lb (840 kg))
Powerplant: 1× Lycoming T53-L-13B turboshaft, 1,400 shp (1,045 kW)

*Performance:
Maximum speed: 135 mph (220 km/h)
Cruise speed: 125 mph (205 km/h)
Range: 315 mi (510 km)
Service ceiling 19,390 ft (Dependent on environmental factors such as weight, outside temp., etc) (5,910 m)
Rate of climb: 1,755 ft/min (8.9 m/s)
Power/mass: 0.15 hp/lb (0.25 kW/kg)

*Armament:
Variable, but may include a combination of:
2x 7.62 mm M60 machine gun, or 2x 7.62 mm GAU-17/A machine gun
2x 7-round or 19-round 2.75 in (70 mm) rocket pods






UH-1C

UH-1D

UH-1E

UH-1N