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Boeing X-50 Dragonfly

Supersonic and Experimental Aircraft

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
Year
2003 1
Engine Class
Jet 1
Status
Destroyed 1
Top Speed (km/h)
700 1
Mass (kg)
574 1
Maximum Mass (kg)
645 1
Engine
Williams F112 turbofan 1
Comparison
Body Style
Aircraft (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, manufacturer
Quote, 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 origin
Quote, 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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