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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]
Seneca then shows that private life (otium) far from being a life of listless retirement can be active from a Stoic point of view. The wise person can choose to engage with the wider universe: by moving one's actions from the local to the cosmic perspective and engage with the fundamental questions of the universe, one can still aid all of ...
The DF Helicopters DF334 is a two-seat, single-engine light utility helicopter in development by Dragon Fly Helicopters [1] in Northern Italy. The DF 334 is a development of the Dragon Fly 333, developed by archaeologists and filmmakers Angelo and Alfredo Castiglioni in the 1980s.
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]
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 .
Data from Cliche and Purdy General characteristics Crew: one Capacity: one passenger Wing area: 500 sq ft (46 m 2) Empty weight: 300 lb (136 kg) Gross weight: 800 lb (363 kg) Fuel capacity: 8 U.S. gallons (30 L; 6.7 imp gal) Powerplant: 1 × Rotax 503 twin cylinder, two-stroke, air-cooled aircraft engine, 50 hp (37 kW) Performance Maximum speed: 30 mph (48 km/h, 26 kn) Cruise speed: 26 mph (42 ...
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 Sukhoi Su-30MKK (NATO reporting name: Flanker-G) [2] is a modification of the Sukhoi Su-30, incorporating advanced technology from the Sukhoi Su-35 variant. The Su-30MKK was developed by Sukhoi in 1997, as a result of a direct Request for tender between the Russian Federation and China. [3]