HAL (Hindustan Aeronautics Limited) of India is developing the "Light Utility Helicopter" (LUH) to fulfill a joint-service requirement for its Army and Air Force calling for a light-class multi-role utility platform. A first-flight was recorded on September 6th, 2016 and the product remains in development with a single example completed. It was originally expected to take to the air during 2015 but delays in the program have seen mounting delays in project goals.
At its core, the helicopter is a traditionally-arranged, rotary-winged aircraft seating the single engine installation over the passenger cabin roof. In the cockpit is seating for two in a side-by-side arrangement. The cabin seats an additional six. Automobile-style doors grant access to the cockpit with sliding doors giving entry/exit to the passenger space. Power is from a HAL (French Turbomeca) "Shakti" Model 1U turboshaft engine delivering 1,706 horsepower to a four-bladed main rotor over the fuselage and a four-bladed tail rotor offset to starboard. Vertical tail fins straddle the tail stem along its midway point and a sole vertical fin sits atop the extreme aft portion of the stem proper. The undercarriage is of a fixed skid-type arrangement, reducing the maintenance commitment, simplifying production and limiting per-unit procurement costs.
To date (2016), the Indian military is contracted for 384 total LUH systems with 187 set to be manufactured by HAL beginning in 2018. Further production will stem from elsewhere.
The LUH is one of several indigenous Indian aviation ventures, showcasing a desire to become more self-sufficient in the field of military equipment. Considering India is one of the top global importers of such goods, it behooves the nation to invest heavily into its own defense.
[ 1 Units ] : Hindustan Aeronautics Limited (HAL) - India
- Commercial Market
- Medical Evacuation (MEDEVAC)
- Search and Rescue (SAR)
- Reconnaissance (RECCE)
52.49 ft (16 m)
43.31 ft (13.2 m)
16.40 ft (5 m)
(Showcased structural dimension values pertain to the HAL LUH (Light Utility Helicopter) production model)
4,211 lb (1,910 kg)
6,945 lb (3,150 kg)
(Showcased weight values pertain to the HAL LUH (Light Utility Helicopter) production model)
1 x HAL (Turbomeca) "Shakti" 1U turboshaft engine developing 1,706 horsepower and driving four-blade main rotor and four-blade tail rotor.
(Showcased powerplant information pertains to the HAL LUH (Light Utility Helicopter) production model)
155 mph (250 kph; 135 kts)
21,325 feet (6,500 m; 4.04 miles)
217 miles (350 km; 189 nm)
1,500 ft/min (457 m/min)
(Showcased performance values pertain to the HAL LUH (Light Utility Helicopter) production model; Compare this aircraft entry against any other in our database)
(Showcased armament details pertain to the HAL LUH (Light Utility Helicopter) production model)
LUH ("Light Utility Helicopter") - Base Series Name
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