Overview

Data on design, manufacture and status

Design authority: Bell Helicopter Company

Primary manufacturer: Bell Helicopter Company

Parent type: Bell Model 209/AH-1 Cobra

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 2

Crew seating: Tandem

Landing gear: Skids

Layout and Dimensions

Data on aircraft size

Airframe width includes stub wings. While there is some variation among Cobra variants, most fuselage widths without stub wings are .914 m (3 ft).

Overall Dimensions
Overall Height: 4.10 m 13.5 ft
Overall Length: 16.14 m 53.0 ft
Overall Width: 13.41 m 44.0 ft
Airframe Dimensions
Airframe Length: 13.77 m 45.2 ft
Airframe Width: 3.15 m 10.3 ft
Airframe Height: 3.11 m 10.2 ft
Landing Gear Dimensions
Landing Gear Base: 3.27 m 10.7 ft
Landing Gear Track: 2.13 m 7.0 ft
Cabin Dimensions
Cabin Internal Height:  
Cabin Internal Length:  
Cabin Internal Width:  

Weights and Performance

Data on aircraft weight and flight characteristics

0

Weights
Max Gross Weight (ground): 4,309 kg 9,500 lb
Max Gross Weight (airborne):  
Max Take-off Weight: 4,309 kg 9,500 lb
Empty Weight: 2,499 kg 5,510 lb
Useful Load: 1,810 kg 3,990 lb
Empty Weight Fraction: 0.580
Climb Performance
Max Rate of Climb: 9 m/s 1,680 fpm
Hover Performance
Hover Ceiling IGE: 3,015 m 9,892 ft
Hover Ceiling OGE: 1,219 m 4,000 ft
Limitations
Max Level Flight Speed: 270 km/h 146 kts
Never Exceed Speed: 352 km/h 190 kts
Service Ceiling: 3,505 m 11,500 ft
Range and Endurance
Max Range: 575 km 310 nm
Max Endurance: 2 hrs 2 hrs

Engine Details

Aircraft powerplant (lift and/or propulsion)

Provided powerplant data is for uninstalled, sea level, static operations.

Powerplant
Number of engines: 1
Designation: Lycoming T53-L-13 turbine
Manufacturer: Lycoming Engines
Normal Ratings
Max continuous: 933 kW 1250 hp
Take-off / rated: 1045 kW 1400 hp
Intermediate:  
Maximum:  
OEI Ratings
OEI contingency:  
OEI continuous:  
OEI 30-second:  
OEI intermediate:  

Primary Lift Device

Data on primary lift devices such as main rotors

B540 blade for two-bladed Cobra main rotors.

Main Rotor Characteristics
Diameter: 13.40 m 43.96 ft
RPM: 324.0 rpm 324.0 rpm
Direction of Rotation: Counterclockwise
Hub Type: Flex-beam, stiff-in-plane teetering hub
Main Rotor Blade Characteristics
Blade Construction: Bonded aluminum spar and skin; nomex honeycomb core
Blade Chord: 0.686 m 2.25 ft
Blade Tip Geometry: Square-edged tips
Blade Twist: -0.175 rad -10.000 deg
Number of Blades: 2
Main Rotor Derived Characteristics
Disc Area: 141.03 m² 1518.0 ft²
Disc Loading: 30.56 kg/m² 6.258 lb/ft²
Solidity: 0.0652
Main Rotor Blade Derived Characteristics
Blade area per blade: 4.59 m² 49.5 ft²
Tip Speed: 227.33 m/s 745.8 fps

Primary Control Device

Data on primary control devices such as tail rotors

Some images show the tail rotor in a 'tractor' type configuration so it appears that configuration changed at some point

Tail Rotor Characteristics
Diameter: 2.59 m 8.50 ft
Configuration: Pusher
Direction of Rotation: Top blade aft
RPM: 1654 rpm 1654 rpm
Tail Rotor Blade Characteristics
Number of Blades: 2
Blade Construction: Bonded aluminum skin with abrasion strip
Blade Chord: 0.213 m 0.70 ft
Blade Twist:  
Tail Rotor Derived Characteristics
Disc Area: 5.27 m² 56.7 ft²
Solidity: 0.1049
Tail Rotor Blade Derived Characteristics
Tip Speed: 224.30 m/s 735.9 fps
Blade Area (per blade): 0.276 m² 2.97 ft²

Related VFS Resources

Resources related to the AH-1G Cobra, provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the AH-1G Cobra, provided by public sources across the internet.

Images