HAL ALH Dhruv Mark I
The Advanced Light Helicopter Dhruv Mark I configuration included mechanical gauges in the (conventional) cockpit, the TM 333-2B2 engine, an Anti-Resonance Vibration Isolation System (ARIS) and Frahm dampers (developed by LORD Corporation). The fuel capacity, useful load and under slung load are 1055 kg, 2490 kg, and 1500 kg, respectively. Passenger capacity is 12-14 plus the crew.
Overview
Data on design, manufacture and statusDesign authority: Hindustan Aeronautics Limited
Primary manufacturer: Hindustan Aeronautics Limited
Parent type: HAL Dhruv
Aircraft status: Operational
Configuration
Primary flight and mechanical characteristicsVTOL 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 featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentReferences
References and sources used14 June 2017
Website
Information Manual Advanced Light Helicopter, circa 1992 (page 8)
Report or Technical Manual
No page numbers in the manual, page numbers marked with very first page being 1.
