Mikoyan MiG-AT
From Wikipedia, the free encyclopedia
| MiG-AT | |
|---|---|
 |
|
| MiG-AT "81" and "83" | |
| Role | Advanced trainer / light attack |
| Manufacturer | Mikoyan |
| First flight | March 16, 1996 |
| Status | Under development |
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.
Contents |
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 March 16 and 22 1996 in Zhukovsky and lasted seven minutes.
Specifications [edit]
Data from Jane's All The World's Aircraft 2003–2004[1]
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 Larzac 04-R-20 turbofan, 14.12 kN (3,170 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 2003, pp. 387–388.
- 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]
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Wikimedia Commons has media related to: Mikoyan-Gurevich MiG-AT |
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