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The Custer CCW-5 was a twin-engined, 5-seat aircraft of pusher configuration, which used a channel wing claimed to enable low speed flight and short take-offs. Two CCW-5s flew, eleven years apart, but the type never entered production. The aircraft was the third and last of a series of Custer Channel Wing designs.
A circulation control wing (CCW) is a form of high-lift device for use on the main wing of an aircraft to increase the maximum lift coefficient and reduce the stalling speed. CCW technology has been in the research and development phase for over sixty years. Blown flaps were an early example of CCW. [1]
Channel Wing aircraft CCW-5. The channel wing is an aircraft wing principle developed by Willard Ray Custer in the 1920s. The most important part of the wing consists of a half-tube with an engine placed in the middle, driving a propeller placed at the rear end of the channel formed by the half-tube. Antonov Izdeliye 181 Experimental
The prototype Custer CCW-1 single-seat test aircraft displayed at the National Air and Space Museum facility at Silver Hill, Maryland in April 1982 Channel Wing concept testing at Langley The first aircraft to incorporate Custer's concept was the CCW-1 which was fitted with a single-seat and was powered by two 75 horsepower (56 kW) Lycoming O ...
Similar to the NASA X-57 Maxwell, the distributed propulsion reduces wingtip vortices and add low speed lift by blowing the wing, enabling a smaller, lower drag wing. [ 12 ] The high voltages required, over 500 volts, is a new challenge in aviation and special cables and protection were developed by Safran.
The United States Air Force's 505th Command and Control Wing is organized under the United States Air Force Warfare Center.The wing is dedicated to improving readiness through integrated training, tactics development and operational testing for command and control of air, space and cyberspace.
Data from Jane's All The World's Aircraft 1953–54. General characteristics Crew: 1 Capacity: 4 passengers Length: 27 ft 5 in (8.36 m) Wingspan: 41 ft (12 m) Height: 10 ft 2 in (3.10 m) Wing area: 207 sq ft (19.2 m 2) Empty weight: 2,200 lb (998 kg) Gross weight: 3,500 lb (1,588 kg) Fuel capacity: 78 US gallons (300 L) Powerplant: 2 × Continental C145-H air-cooled Flat-six engine, 145 hp ...
350th Spectrum Warfare Wing (350 SWW) 505th Command and Control Wing (505 CCW) The 505 CCW is dedicated to improving warfighter readiness through integrated training, tactics, and testing for operational-level command and control of air, space, and cyber power. It hosts the Air Force's only Air Operations Center Formal Training Unit (FTU). [1]