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Mig-AT  
Initial Operational Capability (IOC): 2003
Total Production: ?
Also Known As: Mig-ATC
Origin: France and Russia
Corporations: MiG Corporation
Parent System: Mig-AT
Initial Operational Capability (IOC): 2003
Total Production: ?
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Description: The Mig-AT is a two-seat aircraft designed to provide primary and advanced training for lead-in fighters. It has been developed jointly between the Russian and French defense industries. A redundant fly-by-wire system for enhanced safety and reliability and the HOTAS concept for improved handling qualities have been provided to the Mig-AT trainer aircraft. These features enable the Mig-AT to simulate flight behavior for airborne and ground targets engagements.

The Mig-AT trainer is powered by two French-made Larzac engines rated at 3,150-lb with alternative Russian-made RD-1700 engines. The Mig-AT has been designed to provide training for the Mig-29, Su-27, Mirage 2000, Rafale, Typhoon, F-15, F-16, and F/A-18.

Besides the two-seat Mig-AT aircraft, there are plans to produce the Mig-ATC combat training version featuring a multi-mode radar for precision weapons delivery, a carrier-based version, a single-seat tactical aircraft and a single-seat patrol aircraft. In 2002, the Russian Air Force selected the Yak-130 as the replacement for the older L-29/39 training aircraft.

In August 2005 Svezda company announced that the BKDU-130 oxygen generator system development was completed on the Mig-29M aircraft. The new oxygen generator system was meant to remove the oxygen bottles from Russian manufactured fighter aircraft such as the Mig-29M. Mig-29K, Mig-29KUB, Mig-AT, and Yak-130. Moreover, Svezda stated that there was an agreement between the Russian Air Force and the design bureaus Mig, Yakovlev and Sukhoi on this issue.

Mig-AT Specifications

Crew: 2
Number of Engines: 2
Dimensions
Height: 4.40 meter (14.4 foot)
Length: 12 meter (39.4 foot)
Wingspan: 10 meter (32.8 foot)
Performance
Ceiling: 14,000 meter (45,932 foot)
Max Range: 3,000 kilometer (1,620 nautical mile)
Speed
Top Speed at High Altitude: 237 mps (853 kph)
Weight
Max Takeoff Thrust: 7,500 pound (3,402 kilogram)
Max Takeoff Weight: 8,150 kilogram (17,967 pound)
CEP: Circular Error Probable
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)

Operators & Related Equipment


OperatorsItems

Grand Total ?1
Propulsion Systems
Larzacx2
RD-1700x2
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