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Williams X Jet

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Top speed
  
97 km/h

Engine type
  
Number of seats
  
1

Weight
  
182 kg

Manufacturer
  
Williams X-Jet Hyperborean Vibrations Williams International XJet and other


Similar
  
De Lackner HZ 1 Aerocycle, Hiller VZ 1 Pawnee, Avro Canada VZ 9 Avrocar

Williams x jet


The Williams X-Jet, created by Williams International, was a small, one-man, light-weight, Vertical Take Off and Landing (VTOL) aircraft powered by a modified Williams F107 turbofan aircraft engine designated WR-19-7 after some minor modifications. The vehicle was nicknamed "The Flying Pulpit" for its shape, apparently. It was designed to be operated by / carry one person and controlled by leaning in the direction of desired travel together with the modulation of its input power. It could move in any direction, accelerate rapidly, hover and rotate on its axis, stay aloft for up to 45 minutes and travel at speeds up to 60 miles per hour (97 km/h). In the 1980s, the U.S. Army assessed the X-Jet but found it less capable than helicopters and small unmanned aircraft, leading to the discontinuation of its development.

Contents

Williams X-Jet Williams XJet quotThe Waspquot a technology that never caught on Us

Other VTOL systems developed by Williams International included a jet-powered flying belt, developed in 1969, which was powered by a Williams WR19 turbofan, and X-Jet's predecessor, the WASP I (Williams Aerial Systems Platform) which developed in the 1970s and was powered by the more powerful WR19-9 BRP5 (rated at 670 lbf thrust and a specific fuel consumption of 0.47 lb/(lbf h)).

Williams X-Jet Hyperborean Vibrations March 2011

Specifications (X-Jet)

General characteristics

Williams X-Jet Williams XJet ProofofConcept Prototype Also known as Flickr

  • Crew: One pilot
  • Length: 3ft (m)
  • Wingspan: ft (m)
  • Height: 4 ft 0 in (1.22 m))
  • Wing area: ft² (m²)
  • Empty weight: 401 pounds (182 kg) ()
  • Loaded weight: 550 lb (250 kg)
  • Max. takeoff weight: lb (kg)
  • Powerplant: 1 × modified Williams F107 turbofan, 570 lbf (2.6 kN)
  • Performance

    Williams X-Jet GunBrokercom Message Forums Williams WASP X Jet

  • Maximum speed: 60 mph (96 km/h)
  • Range: endurance of 30-45 minutes ()
  • Service ceiling: 10,000 ft (3,049 m)
  • Rate of climb: ft/min (m/s)
  • Wing loading: lb/(sq ft) (kg/m²)
  • Thrust/weight: 1.11

  • Williams X-Jet httpsuploadwikimediaorgwikipediacommonsthu

    The US PATENT NUMBER 4,447,024 is designated for the Williams X-Jet. Technical information and drawings are available at the United States Patent and Trademark Office. The WASP II uses a slightly modified and derated version of the WR-19-A7D which yields 600 lbf thrust from its micro turbofan engine and is designated WR19-7 ― rated at 570 lbf thrust, after minor modifications and said derating. Modifications to the WR-19-A7D included accessories (replacement of pyro starter with electric/air start) and exhaust system modifications. No internal modifications to the counter-rotating micro turbofans were performed. The first manned, untethered flight was conducted in April 1980. Ray Le Grande is one of the WASP II operators trained by Williams International to fly the X-Jet.

    Williams X-Jet Williams XJet Wikipedia

    Williams X-Jet Williams XJet Any info on Soviet counterparts page 1

    References

    Williams X-Jet Wikipedia