Ilyushin Il-106

Ilyushin Il-106

National origin: Russia
Manufacturer: Ilyushin
Designed by: 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.

Specifications

Data from

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 x— Kuznetsov NK-92 or D-100 turbofan, 176.53 or 186 kN (39685 or lbf) thrust each

Performance

Cruising speed: 850 km/h (528 mph)
Range: 5000 km (3107 miles)

Comparable aircraft

C-17 Globemaster III

Bibliography

Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1 85733 1981 1.

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Source: WikiPedia