Mitsubishi F-2


Mitsubishi F-2A, Japan Air Self-Defense Force, 83-8544, c/n 1044 © Katsunori Kimura
Photo ©: Katsunori Kimura (photos at
The Mitsubishi F-2 is a single-engine single-seat multi-role fighter aircraft produced by the Japanese manufacturer Mitsubishi Heavy Industries.
The Mitsubishi F-2 is a development of the General Dynamics / Lockheed F-16 Fighting Falcon and was developed together with Lockheed Martin. The F-2A is the single-seat version and F-2B is the two-seat version.
Propulsion1 Turbofan Engine
Engine ModelGeneral Electric F110-GE-129
Engine Power
dry/with Afterburner
75,6 / 129,0 kN17000 / 29000 lbf
Speed2124 km/h1147 kts
  1320 mph
Mmo (max. Mach)Mach 2.0
Service Ceiling17.900 m58.727 ft
Rate of climb15300 m/min50197 ft/min
Range833 km450 NM
518 mi.
Empty Weight9.525 kg21.000 lbs
max. Takeoff Weight22.100 kg48.720 lbs
Wing Span11,13 m36 ft 6 in
Wing Area34,8 m375 ft
Length15,52 m50 ft 11 in
Height4,96 m16 ft 3 in
First Flight07.10.1995
Production Statusin production
Developed fromLockheed F-16
Data for (Version)Mitsubishi F-2A
VariantsF-2A, F-2B