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A folding wing is a wing configuration design feature of aircraft to save space and is typical of carrier-based aircraft that operate from the limited deck space of aircraft carriers. The folding allows the aircraft to occupy less space in a confined hangar because the folded wing normally rises over the fuselage decreasing the floor area of ...
SA-11A with folded wings. The SA-11A is a single engine, side-by-side configuration seating, tricycle gear, strut-braced, low wing monoplane. The fuselage is welded steel tubing with aircraft fabric covering. [2] The wings have a quick release mechanism that allows them to fold and lock alongside the fuselage in 15–30 seconds.
The aircraft is a single place, single engine gull-wing design with retractable conventional landing gear. The F4U was the second completed aircraft in the W.A.R. series, with the first example displayed at the EAA airshow in 1975. The aircraft featured folding wings. [3]
A carrier-based aircraft (also known as carrier-capable aircraft, carrier-borne aircraft, or carrier aircraft) is a naval aircraft designed for operations from aircraft carriers. Carrier-based aircraft must be able to launch in a short distance and be sturdy enough to withstand the abrupt forces of launching from and recovering on a pitching deck.
The F2G-1 had manually folding wings and no tail hook, allowing for reduced weight. The F2G-2 had hydraulically powered wing fold mechanisms and tail hooks installed to allow for carrier operations. Armament was to include four or six wing-mounted 0.5-inch (12.7 mm) machine guns and eight 5-inch (127 mm) rockets or two 1,000lbs (454kg) Mk.83 GP ...
Two seat side-by-side seating, high wing, US homebuilt development of the single seat Sparrow UL, with tricycle gear and an optional folding wing for transport or storage, powered by a 64 hp (48 kW) Rotax 582. Empty weight of 510 lb (231 kg) and gross weight 1,050 lb (476 kg). 60 were reported flying in 2004. Production completed.
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Carrier aircraft are at a disadvantage compared to land-based equivalents because they require wing-folding systems increasing the aircraft's weight at the expense of payload. Adaptations of single-engined tail-dragger land-based aircraft typically had poor visibility during landing.