Equipped with Shakti engines, the Advanced Light Helicopter Dhruv Mark III also features a second generation Active Vibration Control System (AVCS) with bi-axial force generators.  

The Weapon System Integrated (WSI) variant of the helicopter is equipped with: armor protection against 12.7 mm rounds; a 20 mm nose-mounted turret gun (by Nexter in France); rocket launcher (FZ, Belgium); air-to-air missiles (MBDA, Fance);, and air-to-ground missiles.  Targeting systems for both day and night include electro-optical pod (Elop, Israel) and Helmet Pointing System (Elbit, Israel).  The aircraft can be fitted with an electronic warfare suite (Avitronics, South Africa), flare/chaff dispensers (BDL, India) and an IR jammer.

Fuel capacity and slung load are 1055 kg and 1500 kg, respectively.  Passenger capacity of the aircraft is 12-14 in addition to the crew.

Overview

Data on design, manufacture and status

Parent type: HAL Dhruv

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 1-2 in Side-by-side arrangement

Landing gear: Skids

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

References

References and sources used

HAL Dhruv
Hindustan Aeronautics Limited
14 June 2017
Website

Hindustan Aeronautics Limited
Hindustan Aeronautics Limited
14 June 2017
Website

Related VFS Resources

Resources related to the ALH Dhruv Mark III, provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.
Images from the VFS Gallery
Enter a search term in the box above.

Related Public Resources

Resources related to the ALH Dhruv Mark III, provided by public sources across the internet.

Images