Mikoyan MiG-AT

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MiG-AT
MiG-AT 81 83.jpg
MiG-AT "81" and "83"
Role Advanced trainer / light attack
Manufacturer Mikoyan
First flight March 16, 1996
Status Cancelled
Number built 2

The Mikoyan MiG-AT is a Russian trainer aircraft that first flew in 1996, designed to replace Aero L-29 and L-39 for the Russian Air Force.

Design[edit]

The MiG-AT is more conventional than the competing Yak-130. It has a low-set, straight wing, engines mounted on either side of the fuselage and a mid-mounted tail. Two prototypes have been built. The first flight took place between 16 and 22 March 1996 in Zhukovsky and lasted seven minutes.

MiG-AT at MAKS-2007 airshow

Flight tests Equipped the AL-55I engine are succeed in 2008.[1]

Specifications[edit]

Data from Jane's All The World's Aircraft 2003–2004[2]

General characteristics

  • Crew: 2
  • Length: 12.01 m (39 ft 5 in)
  • Wingspan: 10.16 m (33 ft 4 in)
  • Height: 4.42 m (14 ft 6 in)
  • Wing area: 17.67 m2 (190.2 sq ft)
  • Aspect ratio: 5.7:1
  • Gross weight: 4,610 kg (10,163 lb) (training)
  • Max takeoff weight: 7,800 kg (17,196 lb) (combat)
  • Fuel capacity: 2,390 L (632 US Gallons)
  • Powerplant: 2 × SNECMA Turbomeca Larzac 04-R-20 turbofan, 14.12 kN (3,170 lbf) thrust each
  • Powerplant: 2 × NPO Saturn AL-55 turbofan, 17.27 kN (3,880 lbf) thrust each
  • Powerplant: 2 × RD-1700 turbofan, 16.67 kN (3,750 lbf) thrust each

Performance

  • Maximum speed: 1,000 km/h (621 mph; 540 kn) at 2,500 m (8,200 ft)
  • Range: 1,200 km (746 mi; 648 nmi)
  • Ferry range: 2,000 km (1,243 mi; 1,080 nmi)
  • Service ceiling: 14,000 m (45,932 ft)
  • g limits: +8.0, -2.0
  • Rate of climb: 81.7 m/s (16,080 ft/min)

Armament

  • Hardpoints: 7 with a capacity of 2,000 kg (4,400 lb) total,

See also[edit]

Aircraft of comparable role, configuration and era

References[edit]

  • Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. ISBN 0-7106-2537-5.

The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.

External links[edit]