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Panha 2091 (Toufan I) Iranian Attack Helicopter

PANHA 2091 (Toufan), IAIO Toufan or Toophan

Attack Helicopter
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Basic Information
Name
Panha 2091 (Toufan I) Iranian Attack Helicopter
Designation
PANHA 2091 (Toufan), IAIO Toufan or Toophan
Alternate Designation
PANHA 2091 (Toufan), IAIO Toufan or Toophan
Equipment Type
Attack Helicopter
Manufacturer
Iran Helicopter Support and Renewal Company (PANHA)
Date of Introduction
1998
Description

The Panha 2091 "Toufan" is an Iranian overhaul and upgrade of the Bell AH-1J International (export version of the SeaCobra) attack helicopter purchased before the 1979 Islamic Revolution. The overhaul and upgrade program is known as project number 2091 of the Iranian Helicopter Support and Renewal Company (also known as Panha). Reported upgrades include: new cockpit armored panels new, Iranian-designed canopy new avionics nose-mounted camera new cockpit design The upgraded attack helicopter has a narrower airframe for greater flexibility and is armed with an M197 three-barreled 20-mm Gatling-type cannon in the A/A49E turret. Its wing-stub stations carry a pair of 19-tube 70-mm rocket launchers. Bulletproof glass protects the pilot's cockpit and weapons officer station, internal avionics have been revamped with the addition of a GPS and receiver in the nose, and a warning radar attached to the rear, with four antennae providing 360 degrees coverage and all electronics systems integrated.

Air & Air Defense Specifications
Crew 2
Engine Turboshaft (1800 hp)
Variants
Toufan II Toufan II unveiled on January 2013
System
Alternative Designation PANHA 2091 (Toufan), IAIO Toufan or Toophan
Type Attack Helicopter
In Service 1998-Present
Manufacturer Iran Helicopter Support and Renewal Company (PANHA)
Crew 2 ea
Blades, Main Rotor 2
Blades, Tail Rotor 2 ea
Number of Engines 1 ea
Day/Night Capable Yes
All Weather Capable INA
Takeoff or Landing Limitations INA
Number of Hard Points INA
Note #1 Developed from Bell AH-1J International Cobra
Note #2 There is little information online about the Panha 2091 (Toufan I)
Dimensions
Length 16 m
Width 13 m
Height 4 m
Weight, Combat 4,530 kg
Weight, Empty 2,802 kg
Automotive
Engine Name 1 x Pratt and Whitney-based Turboshaft Engines
Engine Type Turboshaft Engine
Engine Power 1,800 hp
Cruising Range 600 km
Speed, Maximum 236 km/h
Speed, Average INA
Ceiling 12,000 m
Rate of Climb 494 m/s
Communications
Radio INA
Chin Mounted Gun
System
Name M197 electric cannon
Type 20mm three-barreled electric Gatling-type rotary cannon
In Service 1967-Present
Manufactuer General Dynamics Armament Systems
Barrels 3-barrel (progressive RH parabolic twist, 9 grooves)
Rate of Fire Up to 1500 rpm
Maximum Effective Range INA
Ammunition
Name M53 km
Type API
Caliber 20 mm
Cartidge 20 × 102 mm
Muzzle Velocity 1,030 m/s
Basic Load 2,000 ea
Bursting Charged 4.2 g incendiary
Penetration Penetration 20mm at 25-degree impact and 100 meter range, 6.3mm RHA at 0-degree impact and 1000-m range.
Wing Mounted Weapons
Rocket System
Name Zuni 5-inch Folding-Fin Aircraft Rocket (FFAR)
Type 5in unguided rocket
In Service 1957-Present
Manufacturer United States
Length 2,000 mm
Diameter 130 mm
Warhead Type Various
Engine Solid-fuel rocket
Operational Range 8 km
Speed 2,599 km/h
Guidance System None
Basic Load INA
Missile System
Name AIM-9 Sidewinder
Type Short-range air-to-air missile
In Service 1956-Present
Manufacturer Raytheon Company[1] Ford Aerospace Loral Corp.
Length 3.02 m
Diameter 127 mm
Wingspan 279.4 mm
Weight 85.3 kg
Warhead WDU-17/B annular blast-frag
Warhead Wieght 9.4 kg
Detonation Mechanism IR Proximity Fuze
Engine Hercules/Bermite Mk. 36 Solid-fuel rocket
Operational Range 1-35.4 km
Speed Mach 2.5
Guidance system Infrared homing (most models) semi-active radar homing (AIM-9C)
Fire Control
Fire Control System Type Rocket-launching digital control system
Fire Control Radar Yes
Digital or Analog Cockpit Digital
Direct Fire Control Yes
Laser Designator Yes
Automated Helmet INA
Sensor Suite(s) Available Yes
Position Location System Yes
Central Smart Arms Management System Yes
Multi-Display Monitor, Yes
Protection
Fuselage INA
Cockpit Glass INA
Stealth Properties INA
Heat Signature Reduction INA
Add on Armor INA
NBC Protection Yes
EW INA
EW Counter Measures/CCM INA
Counter Measures (Chaff/Flares) Yes
Details
Country of Origin Iran
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Filter Label
P
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
16 m
Width
13 m
Height
4 m
Weight
4530 kg
Operators (1)
Iran
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