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The HAL Dhruv is a utility helicopter designed and developed by Hindustan Aeronautics Limited (HAL) in November 1984. The helicopter first flew in 1992; 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.
200 HAL Light Combat Helicopters for the Indian Air Force and 500 HAL Dhruv helicopters worth US$5.83 billion. US$900 million aerospace hub in Shamshabad, Telangana. [38] US$57 million upgrade of SEPECAT Jaguar fleet of the Indian Air Force. [39] US$55 million helicopter simulator training facility in Bengaluru in collaboration with Canada's ...
The helicopter is expected to have a maximum take off weight of 13 tonnes and will have 24 to 36 crews on board in various configurations. The helicopter will have a five bladed main rotor with a diameter of 21.2 meters and a four-blade tail rotor. MRH will have 75% domestic content but will use an imported 2000 kW turboshaft engine. Payload ...
The HAL Light Combat Helicopter (LCH) is a multirole combat helicopter, designed to perform various attack profiles, including relatively high altitude flight. [59] The design and development of the LCH was done in-house, by the Rotary Wing Research and Design Centre (RWR&DC), an internal design office of HAL dedicated to the design of helicopters.
The Indian order included an arrangement for the indefinite licence production of the SA 315B to be conducted by Hindustan Aeronautics Limited (HAL) at their facility in Bangalore, India. The first Indian-assembled SA 315B flew on 6 October 1972, with deliveries starting in December 1973; Indian-produced helicopters were given the name Cheetah.
Today, companies like Uber and Hyundai or United Airlines and Archer are working to get fleets of VTOL aircraft to serve as short-hop air taxis, ferrying travelers from city centers to airports ...
The HAL Light Utility Helicopter (LUH) is a 3-tonne class highly agile new generation light helicopter. According to HAL, it possesses a cruise speed of 235 km/h (146 mph), maximum speed of 260 km/h (160 mph), service ceiling of up to 6.5 km (21,000 ft), a range of 350 km (220 mi) with maximum take-off weight of 3.12 tonne and an empty weight ...
The Rudra was expected to attained Initial Operational Clearance (IOC) by late 2012, while deliveries of production helicopters were set to commence by 2013. [15] On 4 February 2013, at the Aero India trade show, it was announced that the HAL Rudra Mk IV had achieved IOC, [16] [17] and that a pair of helicopters had been handed over to the ...