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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 Grumman-patented Sto-Wing aftwards-folding wing folding system, pioneered on the Grumman F4F-4 Wildcat, has been used since World War II on a number of Grumman-designed carrier aircraft, [4] [5] a version of which is still in use in the 21st century on the Grumman E-2 Hawkeye shipboard airborne early warning (AEW) aircraft and its C-2 ...
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 prototype aircraft was built for $287 using tubing from a Cessna UC 78, a Tri-Pacer propeller, wheels from a TG-6 glider, a Lycoming Ground Power unit and a variety of surplus materials. The nickname came from the president of the Experimental Aircraft Association remarking that the plane was a "two holer".
This is a list of United States Navy aircraft wings. The U.S. Navy first used the term "wing" to describe the level of command above its aircraft squadrons when it established five Patrol Wings in 1937. In 1938 it organized the squadrons flying from the five aircraft carriers in commission at the time into Carrier Air Groups.
The Grumman F-14 Tomcat is an American carrier-capable supersonic, twin-engine, two-seat, twin-tail, all-weather-capable variable-sweep wing fighter aircraft.The Tomcat was developed for the United States Navy's Naval Fighter Experimental (VFX) program after the collapse of the General Dynamics-Grumman F-111B project.
The Onex was designed to be economical, have aerobatic capabilities and folding wings, allowing storage in a standard 7 ft (2.1 m) high by 8 ft (2.4 m) wide residential garage. [4] The aircraft has been designed to standard light aircraft FAR-23 static load requirements with the wings supporting more than 10,000 pounds in sandbags during the ...
They began private venture work on unorthodox configurations potentially solving the visibility problem and the complications of folding wings required for storage of ship-borne aircraft. [ 2 ] While contemplating these problems, George Herbert Miles visited the Aeroplane and Armament Experimental Establishment at RAF Boscombe Down .