HAL Dhruv - Specifications (Dhruv)

Specifications (Dhruv)

Data from Indian Army, Crawford, HAL

General characteristics

  • Crew: 1 or 2 pilots
  • Capacity: 12 passengers (14 passengers with high density seating) or 4 stretchers.
  • Length: 15.87 m (52 ft 0.8 in)
  • Rotor diameter: 13.20 m (43 ft 3.7 in)
  • Height: 4.98 m (16 ft 4.06 in)
  • Disc area: 137 m² (1,472 ft²)
  • Empty weight: 2,502 kg (5,515 lb)
  • Useful load: 2,600 kg (5,731 lb)
  • Max. takeoff weight: 5,500 kg (12,125 lb)
  • Powerplant: 2 × Shakti turboshafts, 1,000 kW (1,400 shp)
    Alternate engine: 2 x Turbomeca TM 333-2B2 turboshaft, 746 kW (1,000 shp) each

Performance

  • Maximum speed: 290 km/h (180 mph, 156.58 kn)
  • Combat radius: 320 km (200 mi, 175 nmi)
  • Ferry range: 827 km (516 mi, 447 nmi)
  • Service ceiling: 6,096 m (20,000 ft)
  • Rate of climb: 8.9 m/s (1,771 ft/min)
  • Power/mass: 329.73 W/kg (0.20 hp/lb)

Armament

  • Missiles:
    • 8 Anti-tank guided missiles
    • 4 Air-to-air missiles
    • 4 x 68 mm Rocket Pods (Air-Force & Army)
    • 2 Torpedoes
    • Depth charges or Anti-ship missiles


Note : The Weapon System Integration is in progress and is not in operational service.

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