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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 Piper PA-34 Seneca is a twin-engined light aircraft, produced in the United States by Piper Aircraft.It has been in non-continuous production since 1971. [4] [5] [6] The Seneca is primarily used for personal and business flying [1] as well as multi-engine class rating flight training.
The Dragonfly was a human-powered aircraft, designed and built by the Prestwick Man Powered Aircraft Group, based at the Prestwick International Airport in South Ayrshire, Scotland. [ 1 ] Design and development
Dragonfly HC.4 Casualty evacuation helicopter for the RAF similar to the Dragonfly HR.3 with all-metal rotor blades, 12 built. Dragonfly HR.5 Air-sea search and rescue helicopter for the Royal Navy with Alvis Leonides 23/1 engine and updated to instruments and avionics. 25 modified from HR.1 and HR.3. Westland-Sikorsky WS-51 Mk.1A
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.
With the Bailey engine and the Aeros Discus 15T wing the Dragonfly has an empty weight of 80 kg (176 lb) and a full fuel capacity of 20 litres (4.4 imp gal; 5.3 US gal). With its manual, or optionally electrically retractable landing gear the aircraft can be folded up and ground transported in the trunk of a car. [1]
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