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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 ...
Data from Ultralight News, Pilot Mix. General characteristics Crew: one Capacity: one (ultralight configuration) Length: 17 ft 3 in (5.26 m) Wingspan: 27 ft 5 in (8.36 m) Height: 5 ft 0 in (1.52 m) varies by main landing gear wheel diameter Wing area: 123 sq ft (11.4 m 2) Empty weight: 254 lb (115 kg) Gross weight: 540 lb (245 kg) Fuel capacity: 5 US gallons (19 litres) Powerplant: 1 × Rotax ...
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 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]
The fuselage is wood construction with fabric covering with a folding wing. [3] The pilot and single passenger sit side-by-side in a fully enclosed cabin. One example has been built as a floatplane with fiberglass covered wooden floats using Falconar plans. [4] [5] The airfoil employed is a NACA 23012. [6]
The first production aircraft flew on 22 November 1952. This FJ-2 incorporated further modifications for carrier operations: The track of the main landing gear was widened by eight inches, the outer wing panels folded upward, and the windscreen was modified to give the pilot a better view during approach.
The aircraft is made from metal tubing, with its flying surfaces and fuselage covered doped aircraft fabric. Its 30.00 ft (9.1 m) span wing features Junkers flaperons, has a wing area of 124.5 sq ft (11.57 m 2) and is supported by "V" struts with jury struts. The plans specify standard hydraulic brakes, a steerable tailwheel and wings that fold ...
The T-40 was designed to be a simple to build, all wood aircraft with folding wings. The prototype was modified several times from a single-seat aircraft to a two-place. It also was modified with a bubble canopy and for one flight only, canard control surfaces. [3] The T-40 has conventional landing gear.