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 devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: TBA in Side-by-side arrangement

Landing gear: Wheels (non-retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

References

References and sources used

Vertiflite, Spring 2011, India Special
AHS International
Hirschberg, Mike. "Frome Chetak to Dhruv: The History of HAL Helicopters". Vertiflite, Vol. 57, No. 1. 2011. Print., 2011 (page 48)
Book

Related VFS Resources

Resources related to the Chetan , 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.

Related Public Resources

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

Images