| Specifications |
|---|
| Origin | India.
|
| Type | Advanced multi-role light helicopter.
|
| Length : | 12.89 m
|
| Length | 15.87 meters.
|
| Height : | 3.76 m
|
| Height: 4.98 meters.
|
| Main Rotor Diameter | 13.20 meters.
|
| Weight empty : | 2216 kg / 2502 kg (5515 lbs.)
|
| Max. T/O weight : | 5500 kg (12,125 lbs.)
|
| Cruising speed : | 245 km/h
|
| Max. speed : | 280 km/h / 290 km/h (180 mph)
|
| Climb rate : | 9.00 m/s
|
| Max. Range : | 400 km
|
| Service ceiling : | 6000 m / 5990 metres (19,680 feet)
|
| Engines : | 2x Turboprop Engine - Turboméca TM 333 2B
|
| Power rating : | 1000 wps
|
| Total power rating : | 2000 wps
|
| Payload : | 14pax (max 1500kg)
|
| Useful Load | 2600 kg (5731 lbs.)
|
| Max. cruising speed | 253 km/h (157 mph)
|
| Range |
With 1500 kg (3300 lbs.) payload - 216 nautical miles (414 km; 249 miles).
With max. fuel & 20 min. reserves - 431 nautical miles (810 km; 497 miles).
|
| Fuel Capacity | 1100 kg (2425 lbs.)
|
| Armament | The Army's 'weapons system integrated' helicopters will feature a chin-mounted, three barrel 20mm gun from Lockheed Martin and four pylons - each having two hard points - which will enable it to carry eight Nag anti-tank guided missiles, four 68mm or 70mm rocket pods or four tube-launched air-to-air missiles.
|
| Maximum External Stores Load | 1500 kg. (3307 lb.)
|
| Self Defence | RWR; jammer and chaff/flare dispensers.
|
| Crew : | 2 |
| Important Milestones |
PT1 (Z3182): Official first flight - 30 August 1992 ** An unofficial first flight took place on 20 August 1992.
PT2 (Z3183): First flight - 08 April 1993.
PT3/PT-A (Z3268): First flight - 26 May 1994.
PT4/PT-N (IN901): First flight - 26 December 1995.
|
