Specifications |
---|
Country of Origin | UK
|
Builder | WESTLAND
|
Role | Utility, attack, antitank
|
Similar Aircraft | OH-58 Kiowa, Hirundo A109, UH-1 Iroquois, UH-1N Model 212, Dauphin 2
|
Rotor diameter | 42 ft (12.8 m)
|
Dimensions (External) |
|
Overall Length Rotors Turning |
15. 16 m |
Fuselage Length |
13. 33 m |
Width (excluding rotor) |
2. 94 m |
Overall Height |
3. 48 m |
Folded Length |
10. 85 m |
Folded Width |
2. 94 m |
Folded Height |
3. 25 m |
Main Rotor Diameter |
12. 80 m |
Tail Rotor Diameter |
2. 36 m |
|
|
Dimensions (Internal) |
|
Cabin Length |
2. 05 m |
Cabin Width |
1. 78 m |
Cabin Height |
1. 42 m |
|
|
Accommodation |
|
Cockpit |
Pilot and
Co-Pilot or Observer |
Cabin |
Up to 9
passengers |
Cabin Volume |
4. 85 cu m |
Cabin Floor Area |
3. 45 sq m |
Rotor System |
|
Main Rotor Type |
Semi-rigid |
Main Rotor Blades |
4 composite
blades |
Tail Rotor Type |
Fully
articulated |
Tail Rotor Blades |
4 composite
blades |
|
|
Weights |
|
Maximum All Up Mass |
5330 kg |
Cargo Hook Capacity |
1360 kg |
Standard Fuel |
786 kg |
Auxiliary Fuel Tank |
353 kg each |
|
|
Engines |
|
Number |
2 |
2 |
Make |
Rolls Royce |
LHTEC |
Model |
Gem 42-1 |
CTS800-4N |
Take-Off Rating |
746 kW each |
1015 kW each |
Maximum Continuous |
664 kW each |
945 kW each |
|
|
Performance |
|
Cruise Speed |
137 knots |
Maximum Range (with auxiliary fuel) |
530 nm |
Endurance (with auxiliary fuel) |
5. 4 hours |
Armament | Cannon, minigun, rockets, missiles, HOT or TOW antitank missiles
|
Crew | Two
|
Cost |
|
User Countries | Brazil, Denmark, France, Germany, Netherlands, Nigeria, Norway, UK
|