GlobalMilitary.net Open-source military intelligence Updated daily

Tu-126 Moss

Soviet airborne early warning and control aircraft, developed in the late 1950s and early 1960s, operated during the Cold War from 1965 to 1984. Key figures: top speed 790 km/h, range 7,000 km, service ceiling 10,700 m, max takeoff weight 171,000 kg, built 9.

Max speed
790km/h
Range
7,000km
Produced
9units
Tupolev Tu-126 Moss military special mission aircraft side profile drawing
Side profile · Tupolev Tu-126 Moss · length 56.5 m
Technical SpecificationsVersion: Tu-126
Crew12
Length56.5 m (185.4 ft)
Wingspan51.4 m (168.6 ft)
Height16.1 m (52.7 ft)
Wing area311.1 m² (3348.6 sqft)
Empty weight103,000 kg (227,076 lbs)
Max. takeoff weight171,000 kg (376,990 lbs)
Powerplant4 × Kuznetsov NK-12MV 11,033 kW each
PerformanceVersion: Tu-126
Maximum speed790 km/h (491 mph)
Operational range7,000 km (4,350 mi)
Endurance10 hours
Service ceiling10,700 m (35,105 ft)
Operators — 2026
No country is operating the Tu-126 Moss in 2026.
All Operators
🇷🇺 Ex-USSR

Description

The Tupolev Tu-126 (NATO reporting name: Moss) was a Soviet airborne early warning and control aircraft derived from the Tu-114 airliner by the Tupolev design bureau. It entered service in 1965 and remained operational until 1984, serving as the Soviet Union's first purpose-built AEW&C platform and the predecessor to the Beriev A-50.

Development

The requirement originated in 1958, when concern over an American nuclear strike approaching the USSR from the north created a need for airborne radar coverage in place of a land-based chain along the Soviet northern coast, which would have been prohibitively expensive. The Tupolev Design Bureau was tasked with the design and initially examined installations in the Tu-95 and Tu-116, but both airframes proved too narrow to accommodate operator stations and equipment cooling. The wider fuselage of the Tu-114 was selected instead. The first prototype flew on 23 January 1962. Testing ran through the autumn of 1964 and showed the radar performed adequately over water but poorly over land; the contra-rotating propellers of the four engines also degraded radar performance, a problem only partly addressed by fitting a new radar designated Shmel. Eight production aircraft were built between 1965 and 1968 in addition to the prototype.

Design

The Tu-126 retained the swept-wing, four-engine turboprop layout of the Tu-114, with a length of 56.5 m including the refuelling probe, a wingspan of 51.4 m and a wing area of 311.1 m². Power came from four Kuznetsov NK-12MV axial-flow turboprops of 11,033 kW each, driving eight-bladed contra-rotating propellers. Gross weight was 171,000 kg with 60,800 kg of fuel, giving a range of 7,000 km on internal fuel, an endurance of 10 hours unrefuelled and 20 hours with one in-flight refuelling. Maximum speed was 790 km/h, cruise speed 520 km/h at 9,000 m, and service ceiling 10,700 m. An air-to-air refuelling probe was fitted to meet the range requirement. The primary sensor was the Liana radar (NATO reporting name Flap Jack), housed in a rotodome mounted above the rear fuselage. The radar had no look-down capability. The crew numbered 12, with provision for a full relief crew.

Operational History

The Tu-126 entered service in 1965 but was not identified by Western intelligence until 1968, when it appeared in a Soviet documentary film. All aircraft were nominally based at Šiauliai Air Base. Western assessments rated the radar inferior to Western equivalents, judging it unable to detect cruise missiles or small aircraft at low altitude; the same assessments credited the type with powerful jamming equipment. The NATO shift to low-level penetration tactics reduced the aircraft's utility, as the Liana lacked look-down capability. Operators were the Soviet Air Forces, the Soviet Air Defence Forces and the Egyptian Air Force. The type was replaced by the Beriev A-50, and the last Tu-126 was retired in 1984.

Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 30 August 2026. Suggest a change

Frequently Asked Questions

What type of aircraft is the Tu-126 Moss?
The Tupolev Tu-126 Moss is a military special mission aircraft aircraft developed by Tupolev and entered service in 1965.
What is the maximum speed of the Tu-126 Moss?
The Tupolev Tu-126 Moss has a maximum speed of 790 km/h (490 mph).
What is the range of the Tu-126 Moss?
The Tupolev Tu-126 Moss has an operational range of 7,000 km (4,349 miles). This range can vary based on payload, altitude, and mission profile.
When did the Tu-126 Moss first fly?
The Tupolev Tu-126 Moss made its first flight on January 23, 1962. It entered operational service in 1965.
How many Tu-126 Moss have been built?
9 units of the Tupolev Tu-126 Moss have been produced since it entered service in 1965.
What is the service ceiling of the Tu-126 Moss?
The Tupolev Tu-126 Moss has a service ceiling of 10,700 meters (35,104 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
Compare This Aircraft
Tu-126 Moss vs
Latest Data Updates
  1. AUG 302026 Updated Description updated
  2. JUL 232026 Updated Sources and cross-references refreshed
  3. JUN 302026 Created Page created: Tu-126 Moss