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Il-26
Role	Strategic bomber project
National origin	USSR
Manufacturer	Ilyushin

The Ilyushin Il-26 was a late 1940s project for a strategic heavy bomber by the Ilyushin Design Bureau.^[1]^[2] There were a variety of alternative engines proposed for the Il-26, including the 3,400 kW (4,500 hp) Shvetsov ASh-2TK piston engine and 4,500 kW (6,000 hp) Yakovlev M-501 diesel engine. The specifications varied according to the number and type of engines proposed.

Specifications (Il-26 estimated)

Data from ^[1] Unflown wings : Soviet and Russian unrealized aircraft projects 1925-2010.^[3]

General characteristics

Crew: 12
Length: 39 m (127 ft 11 in)
Wingspan: 61 m (200 ft 2 in)
Height: 13.7 m (44 ft 11 in)
Wing area: 475 m² (5,110 sq ft)
Max takeoff weight: 190,000 kg (418,878 lb)
Powerplant: 6 × Klimov VK-2 turboprop engines, 3,700 kW (5,000 shp) each

Performance

Maximum speed: 545 km/h (339 mph, 294 kn) at sea level

560 km/h (350 mph) at 9,300 m (30,500 ft)

Range: 11,560 km (7,180 mi, 6,240 nmi) with 5,000 kg (11,000 lb) load
Service ceiling: 10,000 m (33,000 ft)

Armament

Guns: 5 x paired 23 mm (0.906 in) cannon in twodorsal, 2 ventral and one tail remote controlled turrets
Bombs: 12,000 kg (26,000 lb) of bombs (maximum)

References

^ ^a ^b Gordon, Yefim; Komissarov, Dmitry; Komissarov, Sergey (2004). OKB Ilyushin. Hinkley: Midland. p. 107. ISBN 978-1-85780-187-3.
^ Buttler, Tony; Gordon, Yefim (2004). Soviet secret projects : bombers since 1945. Hinkley: Midland. pp. 14-15. ISBN 1-85780-194-6.
^ Gordon, Yefim; Komissarov, Sergei (2013). Unflown wings : Soviet and Russian unrealized aircraft projects 1925-2010. Birmingham: Ian Allan Publishing Ltd. pp. 420–421. ISBN 978-1906537340.