The Advanced Light Helicopter Dhruv Mark II features an Integrated Architecture and Display System (IADS) glass cockpit developed with IAI (Lahav Division) to integrate all the avionics, weapons and mission systems.  Fuel capacity, useful load and under slung load are 1055 kg, 2100 kg and 1500 kg, respectively.

Overview

Data on design, manufacture and status

Parent type: HAL Dhruv

Aircraft status: Status unknown

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 (page )
Website

Hindustan Aeronautics Limited
Hindustan Aeronautics Limited
14 June 2017 (page )
Website

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