Bell · United States · ICAO: SUCO · 1966–Onward ·
$10.7 million (2007)

The Bell AH-1 SuperCobra is an attack helicopter manufactured by Bell Helicopter. It is a twin-engine helicopter derived from the single-engine AH-1 Cobra of the United States Army. Its primary users are the United States Marine Corps, the Islamic Republic of Iran Army, the Republic of China Army, and the Turkish Army.

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Engine:
2× General Electric T700-GE-401
Engine type:
Turboshaft
Power:
2 × 1,690 shp  ·  1,260 kW
Avionics:
Northrop Grumman
Wing Tips:
No winglets
Seats:
3
Exterior length:
58 ft 1 in · 17.70 m
Tail height:
14 ft 7 in · 4.44 m
Fuselage diameter:
ft 3 in · 2.20 m
Wing span / rotor:
43 ft 12 in · 13.40 m
Max takeoff weight:
14,700 lb  ·  6,700 kg
Max landing weight:
14,700 lb  ·  6,700 kg
Max Payload:
4,550 lb  ·  2,050 kg
Fuel capacity:
460 gal  ·  1,700 L  ·  1,400 kg  (Jet A)
Max cruise speed:
190 kt  ·  219 mph  ·  352 km/h
Range:
317 nm  ·  360 mi  ·  590 km
Ceiling:
15,000 ft  ·  4,600 m
Rate of climb:
1,614 ft/min  ·  m/s
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Blog Mentions

Blog posts that mention the Bell AH-1 SuperCobra:

The 8 Types of Military Helicopters (with 16 examples)
The 15 Best Attack Helicopters in the World

During the mid-1960s, the AH-1 Cobra began to develop as a temporary gunship helicopter for the United States Army to be used in the Second Indochina War. In June 1967, the delivery of the first AH-1G HueyCobras took place.

From 1967 to 1973, the manufacturing company Bell Helicopter built 1,116 AH-1G helicopters intended for the United States Army. The helicopter completed more than a million operating hours in Vietnam. The AH-1G Cobra gained interest from the United States Marine Corps, however, the USMC favored a twin-engine helicopter for enhanced security and protection in operations over waters, and as well as a more powerful weapon mounted in the turret.

Initially, the Department of Defense hesitantly provided the twin-engine variant of the helicopter to the USMC in the notion that similarity with AH-1G helicopters of the Army exceeded the edge of a dissimilar engine configuration. But in May 1968, the USMC succeeded and signed a contract with Bell Helicopters to produce forty-nine AH-1J SeaCobras equipped with twin-engines. In 1969, the United States Army deployed thirty-eight AH-1Gs to the United States Marine Corps.

The AH-1J SeaCobra can accommodate two crew members. It has an exterior length of 17.7 meters, an exterior height of 4.11 meters, a tail height of 4.44 meters, and a fuselage diameter of 2.2 meters. It has a main rotor diameter of 13.4 meters and a main rotor area of 140.75 square meters. It has a blade section of Wortmann FX 69-H-098.

The twin-engine helicopter is powered by General Electric T700-GE-401 turboshaft engines which produces a maximum thrust of 1,690 horsepower. The helicopter has a maximum cruise speed of 190 knots and a travel range of 317 nautical miles. It can fly up to 15,000 feet and can climb up to a rate of 1,614 feet per minute. The maximum takeoff and landing weights are both 6,690 kg, and the maximum payload is 2,065 kg. The fuel capacity is 460 gallons.

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