A109LUH LIGHT TWIN-ENGINE HELICOPTER
아구스타 웨스트랜드사가 제작한 경량다목적헬기로 남아공이 기존의 알루에트 III헬기를 대체하기위해 30대를 발주하기로 계약했으며 스웨덴도 20대를 발주했습니다.

A109 LUH는 이중의 능력을 보유 군사적 목적이나 의료구급, 정찰 수색 병력수송등에 사용할 수 있습니다.

기존의 A109 헬기 동력계통을 이용하여 제작한 3톤급 경량 쌍발 헬기로 프랑스 터보메카제 Arrius 2K2 형엔진을 장착하여 여유로운 출력을 가지며 최대중량에서도 탁월한 운동성능을 보유하여 폭넓은 무장장착과 임무에 맞는 장비를 갖출 수 있어 진정한 다목적헬기로 사용자의 요구에 맞출 수 있다고 선전합니다.

무장
Rocket launcher 7/12/19 tubes 70/81 mm
Twin machine gun-pod 7.62 mm
Machine gun-pod 12.7/20 mm
Machine gun-pod 12.7 mm with 3 tubes 70 mm rockets
Antitank missiles (TOW, HOT or Hellfire)
Air-to-air missiles (Stinger or Mistral)

장비
External loudspeaker system
Windshield wipers
Reinforced windshields
Wire strike protection system
Bleed air heater
Environmental control unit
1 or 2 longitudinal stretcher installation
Single or dual external cargo hook (1000 Kg/500 Kg)
Rear view mirror
Rescue hoist (270 Kg)
Snow skids
Slump protection pads
Emergency floatation systems
Engine air particle separators
Engine fire extinguishers
Closed circuit refuelling system
SX-16 high intensity search light
External loudspeaker system
Gyro stabilised sight
FLIR / TV sensors
Pilot / copilot armoured seats
Chaff & Flare dispensers
Crashworthy fuel system
Self sealing fuel tanks
Radar warning
Laser warning
Missile approach warning system
Infrared jammer

제원
Weights
Max take Off 3000 kg 6614 lb
Basic Empty Weights 1663 kg 3666 lb
Engine Rating (2 x Pratt & Whitney PW207C)

Take Off power (5 min) 2 x 548 kW 2 x 735 SHP
Maximum continuous power 2 x 466 kW 2 x 625 SHP
O.E.I. Max contingency (2.5 min) 608 kW 815 SHP
O.E.I. Max continuous power 548 kW 735 SHP
Engine Rating (2 x Turbomeca Arrius 2K-2)

Take Off power (5 min) 2 x 530 kW 2 x 711 SHP
Maximum continuous power 2 x 454 kW 2 x 609 SHP
O.E.I. Max contingency (2.5 min) 590 kW 791 SHP
O.E.I. Max continuous power 530 kW 711 SHP
Transmission Rating

Maximum continuous power 671 kW 900 SHP
O.E.I. Max contingency (2.5 min) 477 kW 640 SHP
O.E.I. Max continuous power 418 kW 560 SHP
Fuel Capacity

3 cell fuel system 583 l 154 USG
4 cell fuel system 686 l 181 USG
5 cell fuel system 844 l 223 USG
Crew

Pilot 1 / 2 ?/td> ?/td>
Passengers 6 / 7 ?/td> ?/td> ?/td>
External Dimensions

Length (rotors turning) 13,04 m 42,78 ft
Length (rotors stopped) 11,45 m 37,59 ft
Maximum height 3,50 m 11,48 ft
Main rotor diameter 11,00 m 36,09 ft
Tail rotor diameter 2,00 m 6,56 ft
Performance (MGW ISA-SL)

VNE 311 km/h 168 kts
Cruise speed 290 km/h 156 kts
Rate of climb 8.9 m/sec 1750 ft/min
Hovering IGE 4875 m 16000 ft
Hovering OGE 3050 m 10000 ft
Service ceiling 5650 m 18500 ft
Max Range (1) 890 km 481 NM
Max endurance (1) 4 h 38 min