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The Ilyushin Il-90 was a twin-engine, widebody aircraft proposed by the Ilyushin Design Bureau. First mentioned at the Farnborough air show in 1988, the Il-90 [1] was a replacement for the Ilyushin Il-62M long-range narrowbody airliner. [2] The Il-90 was designed to carry 200 passengers a distance of 5,900 to 7,000 nautical miles (11,000 to 13,000 kilometres; 6,800 to 8,100 miles). On a 540 nmi (1,000 km; 620 mi) sector, per-passenger fuel consumption would be 18 to 19 grams per kilometre (1.0 to 1.1 ounces per mile). [3] Powerplant choices included the NK-92, an 18,000-kilogram-force thrust (177-kilonewton; 40,000-pound-force) ducted propfan engine [4] that was related to the Kuznetsov NK-93. [5]
References
- ^ "Soviets plan new 150-seater" (PDF). Farnborough Report. Flight International. Vol. 134, no. 4131. September 17, 1988. p. 15. ISSN 0015-3710.
- ^ Postlethwaite, Alan (April 18–24, 1990). "Opening doors". Flight International. Vol. 137, no. 4212. pp. 28–31. ISSN 0015-3710.
- ^ "Ilyushin unveils new Il-90 big twin" (PDF). Moscow Aerospace '90. Flight International. Vol. 138, no. 4234. October 3–9, 1990. p. 32. ISSN 0015-3710.
- ^ "Soviet power plants:The Soviet Union's first international aerospace exhibition, held in Moscow in 1990, provided a unique insight into aero-engine industry emerging from the shadows of secrecy". Flight International. January 30 – February 5, 1991. pp. 26–28. ISSN 0015-3710.
- ^ Norris, Guy (July 10–16, 1991). "Soviets team up on 550-seater" (PDF). Headlines. Flight International. Vol. 140, no. 4275. p. 6. ISSN 0015-3710.
 | This article on an aircraft of the 1990s is a stub. You can help Wikipedia by expanding it. |
| This article has multiple issues. Please help
improve it or discuss these issues on the
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Learn how and when to remove these template messages)
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The Ilyushin Il-90 was a twin-engine, widebody aircraft proposed by the Ilyushin Design Bureau. First mentioned at the Farnborough air show in 1988, the Il-90 [1] was a replacement for the Ilyushin Il-62M long-range narrowbody airliner. [2] The Il-90 was designed to carry 200 passengers a distance of 5,900 to 7,000 nautical miles (11,000 to 13,000 kilometres; 6,800 to 8,100 miles). On a 540 nmi (1,000 km; 620 mi) sector, per-passenger fuel consumption would be 18 to 19 grams per kilometre (1.0 to 1.1 ounces per mile). [3] Powerplant choices included the NK-92, an 18,000-kilogram-force thrust (177-kilonewton; 40,000-pound-force) ducted propfan engine [4] that was related to the Kuznetsov NK-93. [5]
References
- ^ "Soviets plan new 150-seater" (PDF). Farnborough Report. Flight International. Vol. 134, no. 4131. September 17, 1988. p. 15. ISSN 0015-3710.
- ^ Postlethwaite, Alan (April 18–24, 1990). "Opening doors". Flight International. Vol. 137, no. 4212. pp. 28–31. ISSN 0015-3710.
- ^ "Ilyushin unveils new Il-90 big twin" (PDF). Moscow Aerospace '90. Flight International. Vol. 138, no. 4234. October 3–9, 1990. p. 32. ISSN 0015-3710.
- ^ "Soviet power plants:The Soviet Union's first international aerospace exhibition, held in Moscow in 1990, provided a unique insight into aero-engine industry emerging from the shadows of secrecy". Flight International. January 30 – February 5, 1991. pp. 26–28. ISSN 0015-3710.
- ^ Norris, Guy (July 10–16, 1991). "Soviets team up on 550-seater" (PDF). Headlines. Flight International. Vol. 140, no. 4275. p. 6. ISSN 0015-3710.
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