Overview
The Mikoyan 1.44, sometimes associated with the MiG-39 or MFI designation, was a prototype developed to demonstrate advanced fighter concepts. Conceived as a response to emerging fifth-generation aircraft, it incorporated stealth shaping and high-performance aerodynamics. The program produced a single flying prototype before cancellation.
Specifications
Units
- Engine
- —
- Engine type
- -
- Thrust
- 39,680 lbf · 177 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 1
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- —
- Tail height
- —
- Fuselage diameter
- —
- Wing span
- —
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 170,000 lb · 77,000 kg
- Max landing weight
- —
- Max payload
- 16,400 lb · 7,450 kg
- Fuel capacity
- Max cruise speed
- 926 kt · 1,066 mph · 1,715 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- —
- Fuel burn
- 0.87 nm/gal · 0.43 km/L
- Ceiling
- —
- Rate of climb
- —
- Takeoff distance
- 400 ft · 120 m
- Landing distance
- 400 ft · 120 m
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