Third prototype Dhruv PT3/PT-A (Z3268).  The Indian Army prototype used the TM 333-2M1 engines.  The fuel capacity of the aircraft is 1,050 kg.

Overview

Data on design, manufacture and status

Design authority: Hindustan Aeronautics Limited

Primary manufacturer: Hindustan Aeronautics Limited

Parent type: HAL Dhruv

Aircraft status: Status unknown

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1-2

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca TM 333 2M1 turbine

Engine manufacturer: Turbomeca

Weights and Performance

Data on aircraft weight and flight characteristics

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Related Public Resources

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