Ilyushin Il-106

From Wikipedia, the free encyclopedia
Jump to: navigation, search


Ilyushin Il-106
Role Heavy military transport
National origin Russia
Manufacturer Ilyushin
Designer G V Novozhilov
Number built None

The Ilyushin Il-106 was a proposed 1990s Russian heavy military transport. It would have been a four-engined high-wing cantilever monoplane with a large 34 m (111 ft 7 in) cabin. [1]

Specifications[edit]

Data from [1]

General characteristics

  • Length: 57.6 m (189 ft 0 in)
  • Wingspan: 58.5 m (191 ft 11 in)
  • Height: 19.93 m ( ft in)
  • Wing area: 370 m2 ( ft2)
  • Empty weight: 135,000 kg ( lb)
  • Gross weight: 258,000 kg (568,792 lb)
  • Useful lift: 80,000 kg ( lb)
  • Powerplant: 4 × Kuznetsov NK-92 or D-100 turbofans, 176.53 or 186 kN (39685 or lbf) thrust each

Performance

  • Cruising speed: 850 km/h (528 mph)
  • Range: 5000 km (3107 miles)
  • Service ceiling: 14,000 m ( ft)

See also[edit]

Aircraft of comparable role, configuration and era

References[edit]

Notes[edit]

  1. ^ a b Taylor 1996, p. 231

Bibliography[edit]

  • Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1-85753-198-1. 

External links[edit]