Rudra is an attack helicopter
manufactured by Hindustan Aeronautics Limited (HAL), for the Indian Army. It is
the Weapon System Integrated (WSI) Mk-IV variant of the Dhruv Advanced Light
Helicopter (ALH). Rudra is the first armed helicopter being produced
indigenously in India.The HAL Rudra helicopter can be deployed in wide range of
missions, including reconnaissance, troop transport, anti-tank warfare and
close air support.HAL was contracted to deliver about 76 Rudra ALH Mk-IV
helicopters for the Indian Army and the Indian Air Force. The Indian Army plans
to equip its Army Aviation Corps with 60 helicopters, forming six squadrons.
HAL handed over the first Rudra helicopter to the Indian Army in February 2013.
Development for the WSI variant was authorised in December 1998. The prototype made its first flight in August 2007. Rudra completed a final round of weapon firing trials in September 2011. The 20mm turreted gun was tested during these trials.The Mistral air-to-air missiles and 70mm rockets were tested on Rudra in November 2011. Mistral is an infrared homing missile, which is capable of striking the targets within a range of 6.5km. The ground tests for the first production helicopter were concluded in September 2012.HAL Rudra Mk-IV received initial operational clearance (IOC) from Centre for Military Airworthiness and Certification (CEMILAC) in February 2013. The helicopter was displayed for the first time at Aero India 2013 show.
The HAL Rudra helicopter is powered by two HAL / Turbomeca Ardiden 1H1 (Shakti) turboshaft engines. Each engine delivers a maximum continuous power of 1,067kW. The operation of the engines is controlled by full authority digital engine control (FADEC) system. The helicopter has a fixed-type metal skid landing gear. The tail section features a tail skid to protect the tail rotor during tail-down landings.The helicopter has a maximum continuous speed of 270km/h. The never exceed speed of the helicopter is 300km/h. Rudra can fly at a maximum altitude of 20,000ft and can climb at a rate of 10.3m/s. It has a range of 660km
Development for the WSI variant was authorised in December 1998. The prototype made its first flight in August 2007. Rudra completed a final round of weapon firing trials in September 2011. The 20mm turreted gun was tested during these trials.The Mistral air-to-air missiles and 70mm rockets were tested on Rudra in November 2011. Mistral is an infrared homing missile, which is capable of striking the targets within a range of 6.5km. The ground tests for the first production helicopter were concluded in September 2012.HAL Rudra Mk-IV received initial operational clearance (IOC) from Centre for Military Airworthiness and Certification (CEMILAC) in February 2013. The helicopter was displayed for the first time at Aero India 2013 show.
HAL Rudra incorporates a
conventional design. Carbon fibre composite materials have been used in
construction to achieve weight reduction. The twin engines mounted above the
cabin are attached to a four-blade composite main rotor. The cockpit is made of
Kevlar and carbon-fibre materials.Rudra has a length of 15.8m, main rotor
diameter of 13.2m and a height of 4.9m. The maximum take-off weight of the
helicopter is 5,500kg. Rudra can carry a payload of 2,600kg.The advanced glass
cockpit of Rudra houses crash-worthy seats for accommodating two crew members.
The night vision goggle (NVG) compatible cockpit is equipped with multifunction
displays, dual flight controls and automatic flight control system.The avionics suite integrates a
global positioning system, FLIR, HF/UHF communications radio, Infrared Friend
or Foe (IFF) identification system, Doppler navigation and a radio altimeter.
The electro-optic pod, helmet-mounted sight and fixed sights ensure the pilots
can accurately engage targets using onboard weapons.
The HAL Rudra helicopter is powered by two HAL / Turbomeca Ardiden 1H1 (Shakti) turboshaft engines. Each engine delivers a maximum continuous power of 1,067kW. The operation of the engines is controlled by full authority digital engine control (FADEC) system. The helicopter has a fixed-type metal skid landing gear. The tail section features a tail skid to protect the tail rotor during tail-down landings.The helicopter has a maximum continuous speed of 270km/h. The never exceed speed of the helicopter is 300km/h. Rudra can fly at a maximum altitude of 20,000ft and can climb at a rate of 10.3m/s. It has a range of 660km
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