Ilyushin Il-90
From The Right Wiki
Jump to navigationJump to search
This article has multiple issues. Please help improve it or discuss these issues on the talk page. (Learn how and when to remove these messages)
|
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.