Ilyushin Il-106
| Ilyushin Il-106 | |
|---|---|
| Role | Heavy military transport |
| National origin | Russia |
| Manufacturer | Ilyushin |
| Designer | G V Novozhilov |
| First flight | 2024-2025 |
| Number built | None |
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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
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
- Aircraft of comparable role, configuration and era
References
Notes
Bibliography
- Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1-85753-198-1.
External links
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