HAL Dhruv Mk III (skid landing gear)
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Explore the HAL Dhruv Mk III (skid landing gear) in side view and top view to compare its silhouette and proportions.
From Wikipedia
The HAL Dhruv is a utility helicopter designed and developed by Hindustan Aeronautics Limited (HAL) in November 1984. The helicopter first flew in 1992; though its development was prolonged due to multiple factors including the Indian Army's requirement for design changes, budget restrictions, and sanctions placed on India following the 1998 Pokhran-II nuclear tests.
Summary of “HAL Dhruv” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
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Drawing of the HAL Dhruv Mk III (skid landing gear) by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/ALH/), CC BY 4.0Specifications
- Length
- 15.87 m52.1 ft
- Rotor diameter
- 13.2 m43.3 ft
- Max take-off weight
- 5.8 t12,800 lb
- Cruise speed
- 250 km/h155 mph
- Range
- 630 km391 mi
- Ceiling
- 6,100 m20,000 ft
- Engines
- 2 × HAL/Turbomeca Shakti -1H turboshaft
- Power
- 1,068 kW (1,432 shp) each (Mk III and IV)
- First flight
- 1992
- In service
- 2002
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.
