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SA 315B Lama, 2003. The Lama was developed specifically to provide a rotorcraft with exceptional high-altitude performance. In practice, the type found considerable use within regions that possessed extensive mountain ranges, such as South America and India, being capable of lifting loads and deploying personnel in areas that had been previously impossible to have otherwise achieved.
Boeing Model 360; Boeing Vertol CH-46 Sea Knight; Boeing CH-47 Chinook; Boeing Vertol YUH-61; Boeing Vertol XCH-62/XCH-62 HLH; Boeing AH-64 Apache; Boeing–Sikorsky RAH-66 Comanche; Boeing X-50 Dragonfly; SkyHook JHL-40; Sikorsky–Boeing SB-1 Defiant
Helicopters with fly-by-wire systems allow a cyclic-style controller to be mounted to the side of the pilot seat. The cyclic is used to control the main rotor in order to change the helicopter's direction of movement. In a hover, the cyclic controls the movement of the helicopter forward, back, and laterally.
The company was renamed Hiller Helicopters in 1948. It was involved in the development of a number of prototype helicopters. It was involved in the development of a number of prototype helicopters. From the early 1960s to 1969, its Palo Alto plant served as a CIA cover for the production of the CORONA reconnaissance satellites .
The Bell 400 TwinRanger featured a reprofiled fuselage, two Allison 250 turboshafts, the OH-58D Kiowa's four-bladed main rotor, and a new shrouded tail rotor. [1] Bell also planned the single-engine 400A, and the 440 twin with a larger fuselage made possible by a high degree of composites. [2] The Bell 400 first flew on April 4, 1984.
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 ...
A Lama V3 model helicopter, with a simplified coaxial rotor system. A recent innovation is that of coaxial electric helicopters. The system's simple direction control and freedom from torque induced yaw have, in recent years, made it a good candidate on small models for beginner and/or indoor use.
The original design for the SW-4 called for it to be powered by a 300 kW (400 shp) PZL Rzeszow GTD350 turboshaft engine, as featured upon the prototype mockup. According to PZL-Swidnik, the early SW-4 could reach the rated top speed of about 240 km/h (130 kn ) and a max range with auxiliary fuel tank about 900 km (485 nmi ).