Overview
The HAL Dhruv is a twin-engine utility helicopter developed by Hindustan Aeronautics Limited in India. Conceived to reduce reliance on foreign designs, it serves in military and civil roles. The aircraft represents a major step in India’s domestic aerospace capability.
Specifications
Units
- Engine
- 2 × Turbomeca TM 333-2B2
- Engine type
- Turboshaft
- Power
- 2 × 1,000 shp · 746 kW
- Avionics
- Israeli-supplied avionics
- Wing tips
- No winglets
- Seats
- 12
- Crew
- —
- Cabin width
- 6 ft 5 in · 1.95 m
- Cabin height
- 4 ft 8 in · 1.42 m
- Cabin length
- 8 ft 10 in · 2.68 m
- Exterior length
- 52 ft 1 in · 15.87 m
- Tail height
- —
- Fuselage diameter
- —
- Wing span
- 43 ft 4 in · 13.20 m
- Baggage volume
- 76 ft³ · 2.2 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 12,100 lb · 5,500 kg
- Max landing weight
- —
- Max payload
- 5,750 lb · 2,600 kg
- Fuel capacity
- 360 gal · 1,400 L · 1,100 kg (Jet A)
- Max cruise speed
- 135 kt · 155 mph · 250 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 346 nm · 400 mi · 640 km
- Fuel burn
- 0.95 nm/gal · 0.46 km/L
- Ceiling
- 14,436 ft · 4,400 m
- Rate of climb
- 2,034 ft/min · 10 m/s
- Takeoff distance
- —
- Landing distance
- —
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