Russia (cancelled)
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
33.3 ft
(10.15 m)
Empty Wgt
9,921 lb
(4,500 kg)
MTOW
17,196 lb
(7,800 kg)
Wgt Diff
+7,275 lb
(+3,300 kg)
(Showcased structural values pertain to the base Mikoyan MiG-AT production variant)
Installed:
2 x SNECMA-Turbomeca "Larzac" 04R20 turbofan engines developing 3,175lb of thrust OR 2 x Aviadvigatel (Soyuz) RD1700 turbofan engines developing 3,750lb of thrust.
Max Speed
621 mph
(1,000 kph | 540 kts)
Ceiling
45,932 ft
(14,000 m | 9 mi)
Range
746 mi
(1,200 km | 2,222 nm)
♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
(Showcased performance specifications pertain to the base Mikoyan MiG-AT production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
Light strike variants were to support gun pods, cannon pods, rocket pods, conventional drop bombs, precision-guided bombs, air-to-air missiles, air-to-surface missiles, and jettisonable fuel tanks across 1 x Centerline and 6 x Underwing (three per wing) external hardpoints.
(Not all ordnance types may be represented in the showcase above)
MiG-AT - Base Project Designation; two flyable prototypes completed.
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.