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RSK MiG MiG-ATType (Muster)Advanced jet trainer and light combat aircraft (Fortgeschrittenentrainer und leichtes Kampfflugzeug)
Country (Land)
Manufacturer (Hersteller)
Phone: 007-095/158-1872 General (Allgemeine Angaben) Crew (Besatzung): 2 in tandem Weapons (Bewaffnung): The MiG-AT has seven hardpoints for up to 2000 kg of external stores, including:
Max. thrust (Schub): 2 x 14,12 kN (3175 lbs) Dimensions (Abmessungen) Length (Länge): 12,01 m Height (Höhe): 4,42 m Wing span (Spannweite): 10,16 m Wing area (Flügelfläche): 17,7 sq m Weights (Massen) Fuel (Kraftstoff): 2390 litres Max. external load (max. Außenlast): 2000 kg Normal take-off weight (normale Startmasse): 4610 kg Max. take-off weight (Max. Startmasse): 7800 kg Performance (Flugleistungen) Max. level speed (max. Fluggeschwindigkeit): 1000 km/h at 2500 m or 850 km/h at sea level Max. Mach number (max. Machzahl): 0.85 Max. rate of climb (Steigrate): 21 m/s at sea level Service ceiling (Dienstgipfelhöhe): 15500 m (50860 ft) Take-off run (Startrollstrecke): 540 m Landing run (Landerollstrecke): 570 m Max. range (Max. Reichweite) - 1200 km at Mach 0.5 - 2600 km on ferry mission g-limits: +8/-2 Costs (Kosten) A price of 12 million US-Dollars was mentioned in 1996. Development costs were estimated by MiG at 200 million US-Dollars in early 2000. Customers (Kunden) None yet. There are hopes that Russia will order the aircraft. Also, export campaigns were undertaken in South Africa and India as well as Greece. Competitors (Konkurrenz) British Aerospace Hawk Yakovlev Yak-130 Remarks (Bemerkungen) The MiG-AT was designed to fulfill a Soviet/Russian requirement for a new generation trainer supplanting the widely used L-39 Albatros. Despite its conservative aerodynamic layout, the MiG-AT features fly-by-wire control which enables the simulation of various aircraft types. The digital FCS is supplied by MNPK Avionika. The programme is supported by Snecma (engines) and Thales (formerly Thomson-CSF, Sextant), which also assist in export efforts. Thales has said that its share of the programme is som 15 per cent, and by mid-2001 it has invested 12 million US-Dollars. History (Geschichte) Design of the MiG-AT started in the late 1980s, in competition with other new trainer projects by Suchoi, Myasichchev and Yakovlev. The Yak-130 and the MiG-AT were choosen as finalists in May 1992. In October 1992, agreements were signed for the supply of French engines and avionics, at least for the prototpyes and pre-series aircraft. Two prototypes have been completed so far:
In November 1996, MAPO MiG signes for ten Larzac 04R20 engines. At that time, 110 test flights had been undertaken. In October 1997, MAPO MiG contracted for the delivery of 20 engines from Snecma and 30 shipsets of nav/attack hardware from Sextant. At that time, a government memorandum was also signed for French financial support for 15 pre-production aircraft. By June 1999, flight time was said to be over 400 hours. An evaluation campaign by the Russian air force is set to start in the autumn of 2002. This should include 370 test flights. Production will take place at the Voronin centre in Moscow. A first batch could be built quickly, with some preparation work on a dozen airframes allegedly under way. The French government has made available a credit line of 400 mio. FF. Minimum launch order necessary is said to be 50 aircraft.
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Home | Update | Latest Issue | GALLERY | FR Inside | Datafiles Copyright 2001 by Motor-Presse Stuttgart. All rights reserved. Last updated 8. August 2001 FLUG REVUE, Ubierstr. 83, 53173 Bonn, Germany |
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