Overview
The Mikoyan MiG-AT was developed as a new-generation jet trainer for modern military pilot instruction. Designed in collaboration with foreign partners, it aimed to replace older training aircraft. The program faced competition and limited production.
Specifications
Units
- Engine
- —
- Engine type
- -
- Thrust
- 1,440 lbf · 6 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 2
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- —
- Tail height
- —
- Fuselage diameter
- —
- Wing span
- —
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 40,300 lb · 18,300 kg
- Max landing weight
- —
- Max payload
- 2,000 lb · 900 kg
- Fuel capacity
- Max cruise speed
- 540 kt · 621 mph · 1,000 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- —
- Fuel burn
- 4.40 nm/gal · 2.15 km/L
- Ceiling
- —
- Rate of climb
- —
- Takeoff distance
- 200 ft · 60 m
- Landing distance
- 480 ft · 150 m
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