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 |
|
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 |
|