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Tupolev Tu-126

Military Aircraft

The Tupolev Tu-126, given the NATO reporting name Moss, was a Soviet airborne early warning and control aircraft built by the Tupolev design bureau on the airframe of the Tu-114 airliner. It was ordered after 1958, when concern over an American nuclear strike from the north created a need for radar cover of the long Soviet northern coast without an enormous chain of ground stations. The wider Tu-114 fuselage solved the cooling and crew space problems met with the narrower Tu-95 and Tu-116, and an air refuelling probe was fitted for range. The aircraft carried the Liana radar in a rotodome above the fuselage and had a crew of twelve. The prototype flew on 23 January 1962, and eight production aircraft followed between 1965 and 1968. The radar had no look-down capability and its performance over land was poor, so it served only until 1984, when the Beriev A-50 replaced it.

Facts
Year
1962 1
Engine Class
Turboprop 1
Status
Retired from service 1
Top Speed (km/h)
790 1
Mass (kg)
103,000 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Tupolev Tu-126 (Wikipedia)

Of Make

Source Tupolev Tu-126 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Tupolev Tu-126 (Wikipedia)Lead, design bureau
Quote, Lead, design bureau
developed from the Tupolev Tu-114 airliner by the Tupolev design bureau

Originated In

Also in Geography Atlas: where this subject originated.

Source Tupolev Tu-126 (Wikipedia)Lead, service
Quote, Lead, service
in service with the armed forces of the Soviet Union from 1965 to 1984
Sources
1. Tupolev Tu-126 (Wikipedia)
  • Design and development, first flight
    The first prototype Tu-126 flew on 23 January 1962
  • Lead
    was an airborne early warning and control aircraft
  • Specifications, powerplant
    Kuznetsov NK-12MV axial flow turboprop engines
  • Operational history, retirement
    The last Tu-126 was retired in 1984
  • Specifications, empty weight
    Empty weight: 103,000 kg
  • Specifications, maximum speed
    Maximum speed: 790 km/h
  • Lead, design bureau
    developed from the Tupolev Tu-114 airliner by the Tupolev design bureau
  • Lead, service
    in service with the armed forces of the Soviet Union from 1965 to 1984
  • Exemplifies: Aviation, Lead, mode
    was an airborne early warning and control aircraft
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