/Air/Japan/Fighters/F-2/Data/F-2.htm | Update: -

 

Mitsubishi F-2 'Viper'

GENERAL DATA
Multirole fighter, air superiority fighter
Mitsubishi Heavy Industries / Lockheed Martin
7 octobre 1995
2000
1995-2011
98 *
In service
1 (F-2A), 2 (F-2B)

(*) including 61 F-2A, 33 F-2B and 4 prototypes

Variants
Single-seat prototypes.
Two-seat prototypes.
Single-seat fighter version.
Two-seat training version.

 

DIMENSIONS
15.52 m
9527 kg (F-2A), 9633 kg (F-2B)
10.8 m *, 11.125 m
13459 kg (clean)
4.69 m
22100 kg
34.84 m²
634.3 kg/m²

(*) without missile launchers

ARMAMENT
1 × 20 mm (0.787 in) JM61A1 Vulcan
6-barrel rotary cannon

512

maximum weapon load of 8085 kg
4 × LAU-61/LAU-68 rocket pods (each with 19/7 × Hydra 70 mm/APKWS[295] rockets, respectively)
4 × LAU-5003 rocket pods (each with 19 × CRV7 70 mm rockets)
4 × LAU-10 rocket pods (each with 4 × Zuni 127 mm rockets)
Air-to-air missiles:


Mitsubishi AAM-3,
Mitsubishi AAM-4,
Mitsubishi AAM-5,
AIM-9 Sidewinder,
AIM-7 Sparrow
Air-to-surface missiles: various free-fall bombs with GCS-1 IIR seeker heads,
JDAM
Anti-ship missiles: ASM-1 and ASM-2 anti-ship missiles
J/AAQ-2 FLIR,
AN/AAQ-33

 

POWERPLANT
1 × General Electric F110-IHI-129 afterburning turbofan
7711 kgp (76.31 kN)
13381 kgp (131kN)
0.606
5678 L internal (3642 kg)*

(*) 1x 1135.5 L + 2x 2271.25 L drop-tanks

PERFORMANCES
2124 km/h (Mach 2) at high altitude
1472 km/h (Mach 1.2) at sea level
? km/h
? m/s
18000 m plus
833 km
1700 km with drop-tanks

 

Sources

 

Drawings

 

 

 

Fighters