Military Aircraft
Overview
The Mikoyan MiG-29M and two-seat M2 are advanced derivatives of the original MiG-29. Designed with improved avionics and airframe refinements, they offer enhanced multirole performance. The aircraft targets both domestic and export customers.
Specifications
Units
- Engine
- —
- Engine type
- -
- Thrust
- 19,840 lbf · 88 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 2 economy · 1 business
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- —
- Tail height
- —
- Fuselage diameter
- —
- Wing span
- —
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 109,000 lb · 49,400 kg
- Max landing weight
- —
- Max payload
- 4,500 lb · 2,050 kg
- Fuel capacity
- Max cruise speed
- 1,350 kt · 1,554 mph · 2,500 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- —
- Fuel burn
- 0.85 nm/gal · 0.42 km/L
- Ceiling
- —
- Rate of climb
- —
- Takeoff distance
- 400 ft · 120 m
- Landing distance
- 500 ft · 150 m
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Operational Context
Mikoyan MiG-29M / M2 — upgraded multirole fighter
The MiG-29M program began in the late 1980s as a comprehensive modernization of the Fulcrum platform. It introduced increased internal fuel capacity, revised aerodynamics, and updated systems. The M2 variant provides a two-seat configuration for training and operational flexibility.
Powered by twin RD-33 series turbofan engines producing around 18,000 to 19,000 pounds of thrust (80 to 84 kN) each with afterburner, the aircraft exceeds Mach 2. Maximum takeoff weight is approximately 50,000 pounds (22,700 kg). It supports a wide range of modern air-to-air and strike munitions.
The MiG-29M and M2 reflect efforts to extend the service life and capability of the Fulcrum family. Improved avionics and structural updates enhance operational effectiveness. The aircraft remains part of Russia’s medium fighter export portfolio.