A version of the Chetak equipped with the more powerful TM 333-2M2 engine.  The max weight and take-off power are 2,100 kg and 825 kW, respectively.

Overview

Data on design, manufacture and status

Design authority: Sud-Aviation

Primary manufacturer: Hindustan Aeronautics Limited

Parent type: No type defined

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: TBA

Crew seating: Side-by-side

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Width: 11.00 m (36.1 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Turbomeca TM 333 2M2 turbine

Engine manufacturer: Turbomeca

Max continuous power: 736 kW (987 hp)

Take-off / rated power: 825 kW (1106 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Range: 580 km (313 nm)

Max Endurance: 3.5 hrs (3.5 hrs)

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Related Public Resources

Resources related to the Chetan , provided by public sources across the internet.

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