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The Dragonfly is a two-seater aircraft that features a tandem wing layout with a forward wing mounted low and the other behind the cockpit in a shoulder position, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed landing gear and a single engine in tractor configuration. The cockpit is 43 in (109 cm) wide [3]
The 201 was a Standard Class sailplane that was a successor to the H-301 Libelle Open Class glider. It was similar to the H-301, with modifications to meet the Standard Class requirements.
The Dragonfly has been incorrectly billed as the world's first commercially available RC ornithopter (flapping wing aircraft). [ citation needed ] It was actually preceded by several other products, including Hobbytechnik's Skybird, Park Hawk, and Slow Hawk radio controlled ornithopters, and the Cybird radio-controlled ornithopter from Neuros.
The media9 LaTeX package enables the production of PDF documents with embedded PRC files using LaTeX. 4D Publish - A plugin for Cinema 4D that exports the scene as a PRC file and embeds it into a 3D PDF document. Teigha PRC library from ODA supports content creation and data access for PRC format and enables exporting a .dwg or .dgn file to PRC.
The Bailey-Moyes Dragonfly is an Australian-American two-seats-in-tandem, high-wing, strut-braced, open cockpit, conventional landing gear-equipped light-sport aircraft. The aircraft has been in production since 1990 and was designed as a special-purpose tug for hang gliders and ultralight sailplanes .
The Boeing X-50A Dragonfly, formerly known as the Canard Rotor/Wing Demonstrator, was a VTOL rotor wing experimental unmanned aerial vehicle that was developed by Boeing and DARPA to demonstrate the principle that a helicopter's rotor could be stopped in flight and act as a fixed wing, enabling it to transition between fixed-wing and rotary-wing flight.
The Dragonfly shares a clear family resemblance with the Dragon Rapide, but is smaller and has higher aspect ratio, slightly sweptback wings.The lower wing has a shorter span than the upper, unlike the DH.89, and the top of the engine nacelles protrude much less above its surface because the fuel tank had been moved to the lower centre section.
The aircraft was designed as a two-place ultralight trainer. It features a parachute-style high-wing, two seats in tandem, tricycle landing gear and a single 50 hp (37 kW) Rotax 503 engine in pusher configuration. The 64 hp (48 kW) Rotax 582 liquid-cooled engine was a factory option. [1] [2] [3]