Jump to content

UTIAS Ornithopter No.1

From Wikipedia, the free encyclopedia
No.1
General information
TypeExperimental ornithopter
ManufacturerUniversity of Toronto Institute for Aerospace Studies
Designer
Number built1
History
First flight8 July 2006

The UTIAS Ornithopter No.1 (registration C-GPTR) is an ornithopter that was built in Canada in the late 1990s. On 8 July 2006, it took off under its own power, assisted by a turbine jet engine, making a flight of around 300 metres that lasted 14 seconds, after which it crashed.[1]

Specifications

[edit]

General characteristics

  • Crew: One pilot
  • Length: 7.47 m (24 ft 6 in)
  • Wingspan: 12.56 m (41 ft 2 in)
  • Gross weight: 322 kg (710 lb)
  • Powerplant: 1 × König SC-430 , 18 kW (24 hp)

Performance

  • Cruise speed: 82 km/h (51 mph, 44 kn)

See also

[edit]

References

[edit]
  1. ^ Hein, Treena (2006-10-12). "CBC News In Depth: Science: The world's first flying ornithopter". CBC News. Retrieved 2010-10-13.
[edit]