HAL Light Combat Helicopter

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Light Combat Helicopter
The HAL LCH final design model
Role Attack helicopter
Manufacturer Hindustan Aeronautics Limited
Status Development
Primary users Indian Air Force
Indian Army
Developed from HAL Dhruv

The HAL Light Combat Helicopter (LCH) is a combat helicopter currently being developed in India by Hindustan Aeronautics Ltd for use by the Indian Air Force and the Indian Army.

The LCH is being designed to fit into an anti-infantry and anti-armour role and will be able to operate at high altitudes (16,300 feet).

HAL hopes to equip the Indian Air Force with about 65 gunships starting 2010.[1] The helicopter will be powered by the Shakti engine developed by HAL, in association with Turbomeca of France. The helicopter will be equipped with helmet-mounted targeting systems, electronic warfare systems and advanced weapons systems.

In 2006, HAL selected the M621 cannon incorporated in a Nexter THL 20 turret for the gun armament of the helicopter, operated by a helmet mounted sight.[2] HAL has completed development of the phase and it will test fly the helicopter by March 2009, a delay of three months from the initial date of December 2008.[3] Three prototypes will be built. The second version will be fitted with weaponry before its test flight. The Indian Air Force will be provided with the third prototype for user trials.[4]

The LCH will incorporate a number of stealth features and crash-worthy landing gear for better survivability. The LCH will have a narrow fuselage, with two crew stations.

The project development cost of LCH is currently pegged at only Rs 376.67 crore since it's basically a derivative of the HAL Dhruv already being inducted into the armed forces. The first prototype's maiden flight in is planned in March 2009, according to HAL LCH should be ready for the initial operational clearance (IOC) by December 2010. With the final operational clearance (FOC) a year or so after that, the newly revised timeframes hold that the 5.5-tonne LCH should be ready for induction into IAF by 2012-2013.[5]

Data from Defense Update[6]

General characteristics

  • Crew: 2
  • Length: 15.8m (51ft 8in)
  • Rotor diameter: 3.55m (11ft 6in)
  • Height: 4.7m (15ft 4in)
  • Disc area: m² (ft²)
  • Empty weight: 2550 kg (5621 lb)
  • Loaded weight: 4000 kg (8818 lb)
  • Useful load: 2950 kg (6503 lb)
  • Max takeoff weight: 5,500 kg (12125 lb)
  • Powerplant: 2× Shakti turboshafts, 900 kW (1200 hp) each

Performance


Armament

Related development

Comparable aircraft

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