Thursday, December 04, 2008

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A-50


Maiden Flight: 1978
IOC: 1982
Total Production: 40


Also Known As
A-50E
A-50EI (Indian Air Force)
A-50M (upgraded version)
Mainstay


Origin
Russia


Contractor/s
Aviadvigatel Perm Engine Company
Beriev
Vega Radio Engineering Corp.

Applications
KJ-2000



Derived from:
Il-76MD

Power plant:
D-30KP (4)
PS-90A (4)

Description: The A-50, Mainstay NATO codename, is an Airborne Warning And Control System (AWACS) aircraft. It is intended to detect and identify airborne and sea objects determining its position, bearing and speed. The objects data collected by the A-50 aircraft is transferred to command centers. In addition, this AWACS aircraft is able to direct aircraft to engage airborne and surface targets. The Soviet Union built around 40 such aircraft in the 1980s with no more than 20 remaining in active service with the Russian Air Force by late 2008.

The A-50 Mainstay aircraft was developed on the basis of Il-76MD military transport aircraft with the radar antenna mounted on the Il-76 fuselage like the NATO E-3 Sentry AWACS aircraft. In fact, the A-50 is the Soviet counterpart to the proven E-3 Sentry aircraft. However, Western Intelligence alleges that the Russian/Soviet aircraft is not that much sophisticated than the E-3 AWACS. It is powered by four D-30KP engines rated at 26,500-lb each. A crew of 10-man is required to manage the whole airborne warning system, while the A-50 aircraft only requires a flight crew of five-man.

The A-50E is the export version and has been sold to China and India. India purchased three A-50EI AWACS which are equipped with the Phalcon radar antenna provided by Israel. The Indian Air Force aircraft are due for delivery beginning from 2009 onwards. The A-50M is a modernized version being carried out by Vega Radio Engineering Corp for the Russian Air Force. Vega is replacing outdated analogue equipment with state-of-the-art digital electronic systems. The A-50M also features aerial refueling equipment and electronic warfare systems. In September 2008, the Russian Air Force started the testing phase for the A-50M aircraft.

Specifications
Accommodation: Crew 15

Dimensions: Height 15 m, Length 46 m, Wingspan 50 m

Weights: Max Weight 190 t

Engine/s Performance: Thrust 106,000 lb (48,082 kg)

Performance: Ceiling 10,200 m (33,465 ft), Endurance 10 hours, Max Detection Range 400 km (216 nm), Max Instrumented Range 800 km (432 nm) not confirmed, Max Range 2,000 km (1,080 nm)

Other: Number of Engines 4, Tracked Aerial Targets 200

Operators

see operators map

China
India / 3
Russia

As of Holdings
2008 20 (from 16-20 aircraft operated by the Russian Air Force)


Image Gallery


Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)


Last Updated: Saturday, November 22, 2008

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