The Ilyushin Il-90 was a twin-engine, widebody airliner proposed by the Ilyushin Design Bureau as a replacement for the Il-62M long-range narrowbody airliner. It was first mentioned at the Farnborough air show in 1988. The design was meant to carry 200 passengers a distance of 5,900 to 7,000 nautical miles, roughly 11,000 to 13,000 kilometres, and on a 540 nautical mile sector its per-passenger fuel consumption was to be 18 to 19 grams per kilometre. The powerplant choices included the NK-92, a ducted propfan engine of 18,000 kilograms-force thrust that was related to the Kuznetsov NK-93. The sources record it only as a proposal and describe no prototype.
Facts
Engine Class StatusDesign only (never built) 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Ilyushin Il-90 (Wikipedia)
Of Make
Source Ilyushin Il-90 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Ilyushin Il-90 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
widebody aircraft proposed by the Ilyushin Design Bureau
Originated In
Also in Geography Atlas: where this subject originated.
Source Ilyushin Il-90 (Wikipedia)Lead, countryQuote, Lead, country
proposed by the Ilyushin Design Bureau
Sources
1. Ilyushin Il-90 (Wikipedia)
Lead
was a twin-engine, widebody aircraft proposed by the Ilyushin Design Bureau
Lead, engine class
Powerplant choices included the NK-92
Lead, manufacturer
widebody aircraft proposed by the Ilyushin Design Bureau
Lead, country
proposed by the Ilyushin Design Bureau
In Group: Wide-Body Airliners, Lead, role
was a twin-engine, widebody aircraft proposed by the Ilyushin Design Bureau
Exemplifies: Aviation, Lead, mode
the Il-90 was a replacement for the Ilyushin Il-62M long-range narrowbody airliner
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