The Tupolev Tu-404 was a

wide-body A wide-body aircraft, also known as a twin-aisle aircraft and in the largest cases as a jumbo jet, is an airliner with a fuselage wide enough to accommodate two passenger aisles with seven or more seats abreast. The typical fuselage diameter is . ...

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blended wing A blended wing body (BWB), also known as blended body, hybrid wing body (HWB) or a lifting aerofoil fuselage, is a fixed-wing aircraft having no clear dividing line between the wings and the main body of the craft. The aircraft has distinct wing ...

jet airliner A jet airliner or jetliner is an airliner powered by jet engines (passenger jet aircraft). Airliners usually have twinjet, two or quadjet, four jet engines; trijet, three-engined designs were popular in the 1970s but are less common today. Air ...

proposed by

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Tupolev Tupolev ( rus, Туполев, , ˈtupəlʲɪf), officially United Aircraft Company Tupolev - Public Joint Stock Company, is a Russian aerospace and Arms industry, defence company headquartered in Basmanny District, Moscow. UAC Tupolev is succes ...

Development

Work on the Tu-404 was initiated in 1991 in parallel with another widebody design, the Tupolev Tu-304. The Tu-404 was designed to transport more than 1,200 passengers to destinations 12,000 - 13,000 km away. The Tupolev Design Bureau investigated several possible configurations for the Tu-404, including a flying wing and a conventional design. The flying wing's powerplant would consist of six pusher turboprop engines developing 18,000 kg of thrust each during take-off and each consuming only 0.644 kg/kgf-h of fuel in cruise mode. The engines would have been located in the tail section of the flying wing fuselage between two large V-shaped vertical stabilizers. The central fuselage contains six passenger compartments accommodating 1214 passengers. The leading edge of the central fuselage has a sweep of 45 degrees. Two large removable wings containing fuel tanks have the leading-edge sweep of 35 degrees and are attached to the central fuselage. The wings hold most of the aircraft's fuel. The conventional design featured a two-level passenger aircraft capable of transporting 1,200 people to destinations of up to 10,000 km. The lower level of the fuselage was designed as a multi-section cargo compartment for transporting cargo in standard aviation containers. Two sub-variants of this design were investigated, a mixed passenger-cargo aircraft with the enlarge cargo section and a dedicated cargo model. The massive low-level wing with a leading-edge sweep of 35 degrees and vertical wingtips has massive control surfaces: multi-section leading-edge control surfaces, low-speed control areas, multi-section flaps. Each half of the altitude control surface is made of two sections. Proposed powerplants included four

Kuznetsov Kuznetsov, Kuznyetsov, Kuznetsoff, or Kouznetsov (masculine, ) or Kuznetsova (feminine, ) is the third most common Russian surname, an equivalent of the English "Smith" (derived from a Russian word ''kuznets'' that means ''blacksmith''). Men * Al ...

NK-44 or Rolls-Royce "Trent" engines installed on underwing pylons. The aircraft's undercarriage consisted of several carts with multiple wheels in each cart. It is retracted into the central fuselage section of the aircraft. The project did not proceed beyond the stage of marketing models.

Specifications (flying wing)

References

{{Tupolev aircraft Tu-404 Abandoned civil aircraft projects Low-wing aircraft Blended wing body

Development

Specifications (flying wing)

See also

References