The fourth Dhruv prototype PT4/PT-N (IN901).  The Indian Navy prototype, this model was equipped with retractable landing gear and the Shakti (Ardiden 1H1 in France) engine. The fuel capacity of the aircraft is 1,108 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: Wheels (all retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca Ardiden 1H1 turbine

Engine manufacturer: Turbomeca

Max continuous power: 650 kW (871 hp)

Take-off / rated power: 741 kW (993 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

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Related Public Resources

Resources related to the Dhruv (PT4), provided by public sources across the internet.

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