The Boeing X-50A Dragonfly, first known as the Canard Rotor/Wing Demonstrator, was an experimental unmanned vertical take-off aircraft developed by Boeing and DARPA to prove that a helicopter rotor could be stopped in flight and then act as a fixed wing. A single turbofan drove the rotor through tip jets for hovering and was switched to a rear nozzle for forward flight, so no tail rotor was needed. A canard foreplane and a conventional tailplane shared the lift in forward flight. Two prototypes were built and the first flight took place on 24 November 2003. The first crashed in March 2004 and the second was destroyed in April 2006, and neither ever completed the transition to forward flight, so DARPA ended funding in 2006.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Of Make
Source Boeing X-50 Dragonfly (Wikipedia)
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Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Boeing X-50 Dragonfly (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
that was developed by Boeing and DARPA
Originated In
Also in Geography Atlas: where this subject originated.
Source Boeing X-50 Dragonfly (Wikipedia)Lead, country of originQuote, Lead, country of origin
developed by Boeing and DARPA
Sources
1. Boeing X-50 Dragonfly (Wikipedia)
Development
The X-50A's maiden flight took place on 24 November 2003.
Lead
rotor wing experimental unmanned aerial vehicle
Development, engine class
The X-50A was powered by a single conventional turbofan engine.
Operation, Crashes
Ship 2 was completely destroyed in a crash at the Yuma Proving Ground on April 12, 2006.
Specifications
Empty weight: 1,265 lb (574 kg)
Specifications, maximum mass
Gross weight: 1,422 lb (645 kg)
Specifications, top speed
Maximum speed: 430 mph (700 km/h, 380 kn)
Specifications, engine
Powerplant: 1 × Williams F112 turbofan
Lead, manufacturer
that was developed by Boeing and DARPA
Lead, country of origin
developed by Boeing and DARPA
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