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Quicky8/19/2023 ![]() ![]() The tandem layout provides positive lift from both pairs of wings whereas on a conventional aircraft, the tailplane mostly provides negative lift. ![]() ![]() Ailerons are located inboard on the rear wing which is shoulder-mounted just aft of the pilot. The full-span control surfaces on the forward wing serve as combined elevators and flaps. ![]() The forward wing provides around 60% of the lift. The wings are foam blanks cut to shape with a hot wire before covering, and the fuselage made up of 1 inch-thick (25.4 mm) foam slabs. Īs with other Rutan designs, the Quickie is constructed of glass fibre and resin over a foam core. According to Rutan this layout was not new, having previously been used in aircraft such as the Mignet "Flying Flea". The Quickie is a tandem wing taildragger, having one forward wing and one rear wing (instead of the more usual main wing and tailplane). An agreement was reached that Rutan would fund the development and testing and once the design was complete they would pay Rutan back from future sales of the designs and kits. Rutan produced the first drawings in May 1977 and thereafter the three of them worked on the design drawings over the next two months with construction beginning in August After the first flights, Rutan spent more time with his Defiant design and other projects, and it was Jewett and Sheehan who continued development of the design and market it for home-build use. The wheels were incorporated into wingtip fairings without much drag penalty and the tandem layout gave safe stalling characteristics. Conversely to canard layout, the conventional front engine location put the pilot close to the center of gravity, a key point for a light aircraft. After a preliminary pusher canard configuration design (Rutan Model 49) had been discarded, his solution to the design issues of low drag without retractable undercarriage and a workable center of gravity travel, was a tractor engine/ tandem wing layout. Rutan was then involved with the design Sheehan and Jewett suggesting a scaled-down Vari-Eze. With the help of Onan, a manufacturer of industrial four-stroke engines, they were able to procure a 70 lb (32 kg) engine that would deliver 18 hp (14 kW) at 3,600 rpm. The first element to be found by Jewett and Sheehan was the engine, which – although low-powered (they had anticipated 12 hp) – had to be reliable for aviation work. The Quickie followed from Jewett and Sheehan's intention in 1975 for a low-cost, low-power, single-seat homebuilt aircraft. The original Quickie (Model 54 in Rutan's design series) is one of several unconventional aircraft penned by Rutan for the general aviation market. Two years later a two-seater variant of the same layout followed as the Q2. The Quickie Aircraft Corporation was formed to produce and market the Quickie in kit form after 1978. The aircraft has unusual landing gear, with the main wheels located at the tips of the forward wing. The forward wing has full-span control surfaces and is thus similar to a canard wing, but is considerably larger. Its tandem wing design has one anhedral forward wing and one slightly larger dihedral rear wing. The Quickie was primarily designed by Burt Rutan as a low-powered, highly efficient kit-plane. The Rutan Quickie is a lightweight single-seat taildragger aircraft of composite construction, configured with tandem wings. ![]()
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