| Weights |
|
| Max take Off | 6000 kg 13228 lb
|
| Engine Rating | (2 x LHTEC CTS800-4N)
|
| Take Off | 1014 kW 1361 shp
|
| Fuel Capacity | Standard 1004 l 221 USgal
|
| Crew | Pilot/ Passengers 2/6
|
| External Dimensions |
|
| Length (rotors turning) | 15.24 m 50.0 ft
|
| Overall height | 3.73 m 12.3 ft
|
| Main rotor diameter | 12.80 m 42.0 ft
|
| Performance (At MTOW - ISA) |
|
| Max speed | 296 km/h 160 kts
|
| Hovering IGE | 2587 m 8488 ft
|
| Hovering OGE | 1858 m 6097 ft
|
| Max endurance (internal fuel) | 2 h 40 mins
|
| Equipment |
Aircrew and passenger crashworthy seating
Armoured crew seats and armoured floor
Rescue hoist
Waterproof floor installation
Cargo hook
Stretchers
Rappelling/ fast roping kit
Harpoon decklock
Wire strike protection system
IR engine exhaust suppression system
Four bag emergency flotation system
|
| Avionics |
HUMS
Electro Optical Device
Electronic Support Measures
360 degree AESA surveillance radar
Integrated surface Automatic Identification System (AIS)
Tactical Data Link
Anti Submarine Warfare (ASW) Active Dipping Sonar
Digital map
Defensive Aids Suite
|
| Armament |
Forward firing cannon
7.62/12.7mm pintle mounted machine gun
Air-to-surface rockets
Air-to-surface missiles
Torpedoes
Depth charges
|
