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AH-1W Super Cobra American Attack Helicopter

AH-1W SuperCobra

Attack Helicopter
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Basic Information
Name
AH-1W Super Cobra American Attack Helicopter
Designation
AH-1W SuperCobra
Alternate Designation
AH-1W SuperCobra
Equipment Type
Attack Helicopter
Manufacturer
Bell Helicopter
Date of Introduction
1986
Description

The AH-1W, the backbone of the United States Marine Corps. Marines have been flying the AH-1W Super Cobra since 1986. The last AH-1W was delivered in 1998. AH-1Ws are fielded in Marine Light Attack Helicopter Squadrons or HMLAs. Detachments from HMLAs deploy as part of the task-organized Aviation Combat Element of a Marine Air-Ground Task Force, the most common of which is the Marine Expeditionary Unit, or MEU. The Super Cobra was the first attack helicopter to qualify both the Sidewinder air-to-air missile and the Sidearm anti-radiation missile. Both missiles can use the same LAU-7 rail launcher. Sidearm has a range of more than 15km. AIM-9L Sidewinder is an all-aspect, short-range, air-to-air missile produced by Lockheed Martin and Raytheon. The missile has a range of 15km. A major upgrade of the Bell Super Cobra known as the H-1 program is underway. The program calls for the re-manufacture of the US Marine Corps fleet of 180 AH-1W Super Cobra and 100 UH-1N utility helicopters to an advanced four-bladed configuration, which will operate beyond 2020.

Air & Air Defense Specifications
Engine Turboshaft (1725 hp)
Endurance 3.00 hrs
Service Ceiling 3 m
Variants
AH-1J SeaCobra Original twin engine version.
AH-1J International Export version of the AH-1J SeaCobra.
AH-1T Improved SeaCobra Improved version with extended tail boom and fuselage and an upgraded transmission and engines.
AH-1(4B)W Viper "Four-Bladed Whiskey" test version with a four-bladed bearingless composite main rotor based on Bell 680 rotor. A prototype was converted from AH-1T 161022.
AH-1Z Viper A new variant nicknamed "Zulu Cobra", and developed in conjunction with the UH-1Y Venom for the H-1 upgrade program. The variant includes an upgraded four-blade main rotor and adds the Target Sight System (TSS).
Bell 309 KingCobra Experimental all-weather version based on the AH-1G single-engine and AH-1J twin-engine designs.[36] Two Bell 309s were produced; the first was powered by a PW&C T400-CP-400 Twin-Pac engine set and the second was powered by a Lycoming T-55-L-7C engine.
CobraVenom Proposed version for the United Kingdom.
AH-1Z King Cobra AH-1Z offered for Turkey's ATAK program; selected for production in 2000, but later canceled when Bell and Turkey could not reach an agreement on production.
Panha 2091 Unlicensed Iranian upgrade of AH-1J International.
IAIO Toufan Iranian copy / re-manufactured AH-1J International by Iran Aviation Industries Organization, with locally sourced avionics, and weapons.
System
Alternative Designation AH-1W SuperCobra
Type Attack Helicopter
Manufacturer Bell Helicopter
In Service 1986-Present
Crew two: pilot, co-pilot/gunner
Cockpit Configuration Two seats, in tandem (pilot in rear, copilot/gunner in front)
Blades, Main Rotor 2 ea
Blades, Tail Rotor 2 ea
Number of Engines 2 ea
Day/Night Capable Yes
All Weather Capable Yes
Takeoff or Landing Limitations INA
Number of Hard Points 4 ea
Landing Skids Yes
Dimensions
Fuselage Length 13.9 m
Main Rotor Diameter 14.63 m
Height 4.32 m
Weight, Maximum Take Off 6.69 tons
Weight, Empty 4.6 tons
Disc Area 168.1 m²
Stub Wing Span 3.28 m
Automotive
Engine Name 2 x General Electric T700-GE-401 turboshafts
Engine Type Turboshaft
Engine Power 1725 hp for each engine
Fuel Capacity 1154.55 liters
Cruising Range 587-635 km
Speed, Maximum 315 km/h
Speed, Crusing 281 km/h
Service Ceiling 3.72 km
Rate of Climb 8.2 m/s
Ceiling 5,486 m
Hover IGE 4,267 m
Hover OGE 792 m
Endurance 3 hours
Note The second engine offers additional backup, as in case of failure or damage, the helicopter can still limp back home with one engine working
Chin Mounted Gun
System
Name 1 x M61 Vulcan
Type Hydraulically, electrically or pneumatically driven, six-barrel, air-cooled, electrically fired Gatling-style rotary cannon
Caliber 20 mm
Manufacturer General Dynamics
In Service 1946-Present
Length 1.827 m
Weight, With Feed System 112 kg
Weight, Without Feed System 92 kg
Barrels 6-barrel (progressive RH parabolic twist, 9 grooves)
Action Hydraulically operated, electrically fired, rotary cannon
Rate of Fire, M61A1 6,000 rds/min
Rate of Fire, M61A2 6,600 rds/min
Feed System Belt or linkless feed system
Note #1 The turret can pivot to both sides of the helicopter, as well as up and down.
Note #2 The Super Cobra can carry additional pods with miniguns on stub wings.
Ammunition
Name M53
Type HEI
Caliber 20 mm
Cartridge 20×102 mm
Muzzle Velocity 1,050 m/s
Armor Penetration 6.4 mm (0.25 in) RHA penetration at 0 degree impact angle and 1,000 m (3,300 ft) range
Basic Load 750 round
Note The M61 Vulcan can also fire M56A3/A4 and PGU-28A/B 20mm rounds
Wing Mounted Weapons
Additional Weapons the AH-1H can carry 8 x AGM-71 TOW anti-tank missiles; or 2 x AGM-122 Sidearm anti-radar missiles; or 8 x AGM-114 Hellfire anti-tank missiles; or 4 x CMU-55B fuel-air explosive weapons; or 16 x 5-in (127-mm) Zuni rockets; or 4 x 78 gal (295-liter) auxiliary fuel tanks; or 2 x 100 gal (378-liter) auxiliary fuel tanks
Anti-Tank Guided Missile System
Name AGM-114 Hellfire
Type Anti-Tank Guided Missile (ATGM)
Manufacturer Lockheed Martin, Boeing (previous second source), and Northrop Grumman (seeker only for AGM-114L Longbow Hellfire)
In Service 1984-Present
Length 1.6 m
Wingspan 330 mm
Diameter 180 mm
Weight 45-49 kg
Warhead Type High-explosive anti-tank (HEAT)
Engine Solid-fuel rocket
Operational Range 0.499–11.008 km
Speed Mach 1.3
Guidance system Semi-active laser homing millimeter wave radar seeker
Launch Platform Rotary- and fixed-wing platforms, unmanned combat air vehicles, tripods, ships, and ground vehicles
Basic Load 4 ea, one on each hardpoint ea
Note The Super Cobra is also armed with Hellfire or TOW anti-tank guided missiles. It can actually carry both types of missiles on the same mission.
Air-to-Air Missile
Name AIM-9 Sidewinder
Type short-range air-to-air missile
Length 3.02 m
Diameter 127 mm
Wingspan 279.4 mm
Manufacturer Raytheon Company[1] Ford Aerospace Loral Corp.
In Service 1956-Present
Weight 85.3 kg
Warhead Type WDU-17/B annular blast-frag
Warhead Weight 9.4 kg
Detonation Mechanism IR proximity fuze
Engine Hercules/Bermite Mk. 36 Solid-fuel rocket
Operational Range 1.0 to 35.4 km
Speed Mach 2.5
Guidance system Infrared homing (most models) semi-active radar homing (AIM-9C
Launch platform Aircraft, naval vessels, fixed launchers, and ground vehicles
Basic Load 4 ea, one on each hardpoint
Note The Super Cobra can also carry AIM-92 Stinger short-range air-to-air missiles, and AGM-122 Sidearm anti-radiation missiles. This gunship also has provision for AGM-65 Maverick air-to-ground missiles.
Rockets and Bombs
Note The SuperCobra can also carry various pods with unguided rockets, cluster munitions, napalm bombs
Fire Control
Fire Control System Yes
Fire Control Radar Yes, type INA
Digital or Analog Cockpit INA
Direct Fire Control Yes
Laser Designator Yes
Laser Rangefinder Yes
Sensor Suite(s) Available Yes, low speed air data sensor
Position Location System Yes
Forward-Looking Infra-Red (FLIR) Yes
TV Camera Low-light TV camera
Autotrack System Yes
Night Targeting System (NTS) Yes
Thermal Sights thermal sights and a FLIR to allow for acquisition, launch, and tracking of all types of TOW missiles in all weather conditions
Digital Ballistic Computer Yes
Heads Up Display Yes
Navigation Doppler navigation
In Flight Boresighting Yes
Protection
Fuselage Type The Super Cobra has a slim fuselage with a fighter-type cockpit
Cockpit Protection The cockpit is surrounded by armor protection. Armored cockpit can withstand small arms fire.
Tailboom Protection Tail boom are able withstand damage from 23-mm cannon hits.small arms fire, and composite blades and tailboom able to withstand damage from 23-mm cannon hits.
Stealth Properties No
Heat Signature Reduction INA
Add on Armor INA
NBC Protection Yes
EW INA
EW Counter Measures/CCM INA
Counter Measures (Chaff/Flares) AN/ALE-39 Chaff system and SUU-4/1 Flare dispensers
Details
Country of Origin United States
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Filter Label
A
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
Height
4.32 m
Weight
6690 kg
Operators (6)
China
United States
Turkey
Iran
Taiwan
CFE Treaty
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