Bell AH-1 Cobra

$11.3 million attack helicopter

Israeli AH 1 Cobra
photo: Oren Rozen

The Bell AH-1 Cobra is a single-engine attack helicopter introduced in 1967. It was manufactured by Bell Helicopters and was the fundamental part of the fleet of attack helicopters of the United States Army. The engine, transmission, and rotor system of the AH-1 Cobra were derived from the UH-1 Iroquois utility military helicopter.

Manufacturer:
Bell Helicopter
Country:
United States
Manufactured:
1967 to: 2019
ICAO:
HUCO
Price:
US$11.3 million (1995)

Specifications

Avionics:
Engine:
1x Lycoming T53-L-13
Turboshaft
Power:
1,100 horsepower
Max Cruise Speed:
149 knots
276 Km/h
Approach Speed (Vref):
Travel range:
310 Nautical Miles
574 Kilometers
Fuel Economy:
Service Ceiling:
11,400 feet
Rate of Climb:
1230 feet / minute
6.25metre / second
Take Off Distance:
Landing Distance:
Max Take Off Weight:
4,309 Kg
9,500 lbs
Max Landing Weight:
Max Payload:
Fuel Tank Capacity:
Baggage Volume:
Seats - Economy / General:
2 seats
Seats - Business Class:
Seats - First Class:
Cabin Height:
Cabin Width:
Cabin Length:
Exterior Length:
16 metre - 52.49 feet
Tail height:
4.08 metre - 13.39 feet
Fuselage Diameter:
1.06 metre - 3.48 feet
Wing Span / Rotor Diameter:
13.4 metre - 43.96 feet
Wing Tips:
No Winglets
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Description

On September 7, 1965, the AH-1 prototype designated as Model 209 took to the skies for the first time. In April 1966, the Model 209 gained a successful evaluation in opposition to contesting helicopters. Afterward, the United States Army signed a contract for the delivery of one hundred and ten helicopters. The Model 209 has been in use for the next six years in testing armaments and equipment.

The Bell AH-1 Cobra has a length of 16 meters including rotors, a fuselage length of 13.5 meters, an exterior height of 4.11 meters, a tail height of 4.08 meters, and a width of 3.15 meters with stub wings. The main rotor diameter is 13.4 meters and the man rotor area is 141 square meters. It has a blade section of NACA 0009.3 mod.

The helicopter is powered by a single T53-L-13 turboshaft engine designed by Lycoming at the Lycoming Turbine Engine Division in Stratford, Connecticut. It is a turboshaft type with a 5-stage axial and 1-stage centrifugal compressor, a reverse flow combustor, and a 2-stage high pressure and 2-stage power turbine. It produces a maximum thrust of 1,100 horsepower. It has a length of 1.5 meters and a diameter of 0.5 meters.

The Cobra has a maximum speed of 149 knots and a never exceed speed of 190 knots. The travel range is 310 nautical miles. It can fly up to 11,400 feet and can climb at a rate of 1,230 feet per minute. The maximum takeoff weight is 4,309 kg while the empty weight is 2,635 kg.

The AH-1 Cobra could be loaded with various armaments such as 2×7.62 mm multi-barrel Miniguns or 2 x M129 40 mm grenade launchers, or one of each weapon in the M28 turret. It can also be loaded with 70 mm rockets- seven rockets fitted in the M158 launcher or nineteen rockets fitted in the M200 launcher, and M18 7.62 mm Minigun pod or XM35 armament subsystem with XM195 20mm cannon.

All Bell Helicopter Aircraft

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