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The helicopter was designated "CH-53A Sea Stallion" and delivery of production helicopters began in 1966. [5] The first CH-53As were powered by two General Electric T64-GE-6 turboshaft engines with 2,850 shp (2,125 kW) and had a maximum gross weight of 46,000 lb (20,865 kg), including 20,000 lb (9,072 kg) in the payload.
The Sikorsky CH-53K King Stallion (Sikorsky S-95) [2] is a heavy transport helicopter designed and produced by Sikorsky Aircraft.The King Stallion is an evolution of the long running CH-53 series of helicopters which has been in continuous service since 1966, and features three up-rated 7,500 shp (5,590 kW) engines, new composite rotor blades, and a wider aircraft cabin than its predecessors.
Their transport helicopters are the most-used in the Army currently. [12] Up to 2013, Sikorsky and partners have spent $250 million on X2 and Raider. [6] The team and aircraft will be separate from the S-97 Raider. [10] The team feels confident in the SB-1 Defiant and is paying for more than half of its design costs.
The Mi-26 was designed to replace earlier Mi-6 and Mi-12 heavy lift helicopters and act as a heavy-lift helicopter for military and civil use, having twice the cabin space and payload of the Mi-6, then the world's largest and fastest production helicopter.
Its [The V-22's] production costs are considerably greater than for helicopters with equivalent capability – specifically, about twice as great as for the CH-53E, which has a greater payload and an ability to carry heavy equipment the V-22 cannot ... an Osprey unit would cost around $60 million to produce, and $35 million for the helicopter ...
The high cost is the price of maintaining the airplane’s leading-edge capabilities, including its anti-radar stealth and F119 high-performance engines. ... The tank-killing AH-64 Apache attack ...
The Block 2 aims for a payload of 22,000 lb (10,000 kg) with 4,000 ft (1,200 m) and 95 °F (35 °C) high and hot hover performance, eventually increased up to 6,000 ft (1,800 m), to carry the Joint Light Tactical Vehicle; maximum takeoff weight would be raised to 54,000 lb (24,500 kg).
From 1981 to 1987, five Black Hawks crashed (killing or injuring all on board) while flying near radio broadcast towers because their electromagnetic emissions disrupted the helicopters' flight control systems. The Black Hawk helicopters were not hardened against high-intensity radiated fields, contrary to the SH-60 Seahawk Navy version. The ...