The F-2 is a direct offshoot of the proven American F-16 'Fighting Falcon' design developed to suit a Japanese requirement for a multirole performer. Nearly 100 of the type were produced in both single- and twin-seat forms and the series continues to see service today. MHI is responsible for 60% of manufacturing with the remainder handled by Lockheed Martin. Production spanned from 1995 to 2011.
1+(1) CREW
Speed
1,320 MPH
Ceiling
49,213 FEET
Range
2,610 MILES
Mission Roles
AIR-TO-AIR
INTERCEPTION
GROUND ATTACK
STRIKE
ANTI-SHIP
ANTI-RADAR
RECON
TRAINING
UNMANNED
EXPERIMENTAL
Gallery
1 / 5
Image from the US DoD DVIDS imagery database; released to the public.
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Image from the US DoD DVIDS imagery database; released to the public.
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Image from the US DoD DVIDS imagery database; released to the public.
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Image from the US DoD DVIDS imagery database; released to the public.
5 / 5
Image from the US DoD DVIDS imagery database; released to the public.
Operational Range 2,610 miles | 4,200 km | 2,268 nm
Rate-of-Climb 59,000 ft/min | 17,983 m/min
(Showcased performance statistics pertain to the F-2A production model)
Length 50.92 feet (15.52 meters)
Width 36.52 feet (11.13 meters)
Height 16.08 feet (4.90 meters)
(Showcased measurements pertain to the F-2A production model)
Empty 21,010 lb (9,530 kg)
M.T.O.W. 48,722 lb (22,100 kg)
(Showcased weights pertain to the F-2A production model)
Ordnance and special-mission equipment mounted at 3 x Fuselage hardpoints (1 x Center; 2 x Side), 6 x Underwing hardpoints (3 per wing), and 2 x Wingtip hardpoints (1 per wing). Supported Types:
Close-in Gun(s)
Air-to-Air Missiles
Air-to-Surface Missiles
Precision-Guided Bombs
Conventional Drop Bombs
Rockets / Rocket Pods
Additional Fuel
F-2 - Base Series Designation.
XF-2A - Single-seat flyable prototype.
XF-2B - Twin-seat flyable prototype.
F-2A - Single-seat production version; fighter form.
F-2B - Twin-seat production version; trainer form.
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