|
Entered service |
2001 |
|
Crew |
1 men |
|
Dimensions and weight |
|
Length |
15.52 m |
|
Wing span |
11.13 m |
|
Height |
4.69 m |
|
Weight (empty) |
9.53 t |
|
Weight (maximum take off) |
22.1 t |
|
Engines and performance |
|
Engines |
1 x General Electric F110-GE-129 turbofan |
|
Traction (dry / with afterburning) |
75.62 / 131.22 kN |
|
Maximum speed |
2 125 km/h |
|
Combat radius |
> 843 km |
|
Armament |
|
Cannon |
1 x 20-mm JM61A1 cannon |
|
Missiles |
ASM-1/2 anti-ship missiles, AIM-7F / AIM-7M+
Sparrow, AIM-9L or AA-3+ air-to-air missiles |
|
Bombs |
Mk 82 and JM117 free-fall bombs with infra-red
seeker heads, CBU-87/B cluster bombs |
|
Other |
JLAU-3/A and RL-4 rocket launchers |
|
In October 1987, Japan selected the
F-16C Fighting Falcon as the
basis for a much developed version to replace the Mitsubishi F-1,
primarily in the fighter support role. Although a costly ad
controversial programme - one F-2 costs at least the same as four
Block 52/52 F-16Cs - the F-2 illustrates Japan's commitment to
maintaining its high-technology aerospace industry.
The F-2 features a new wing of 25 per cent greater-area and
co-cured, all-composite construction, with radar absorbent material
on the leading edges. In order to house additional mission avionics
that include an integrated electronic warfare system, the F-2's
fuselage has a lengthened forward section when compared to the
F-16C. Other features include a longer nose to accommodate an active
phased-array radar, a larger tailplane, a brake chute and a
strengthened canopy.
Mitsubishi is the prime contractor responsible for airframe assembly
as well as manufacture of the forward fuselage section, while the
other major assemblies are produced by Lockheed Martin, Kawasaki and
Fuji. With either wing tip-mounted AIM-9 or Mitsubishi AAM-3
air-to-air missiles, the F-2 still has 11 hardpoints available for
other stores, including the ASM-2 anti-ship missile as one of the
principal weapons. The F-2 programme has suffered long delays, cost
escalation and a number of structural problems including wing
cracking and severe flutter. Four prototypes have been built
comprising two single-seat XF-2As and a pair of two-seat XF-2B.
The first XF-2A recorded the type's maiden flight on 7 October 1995.
In late 1995 the Japanese government approved a programme for the
manufacture of 130 aircraft with an entry into service scheduler for
1999. Delays resulting from modifications to cure structural
problems delayed the F-2's entry into operational service until
2001. The current production programme calls for production of 83
F-2A single-seaters and 47 F-2B two-seaters. Retaining full combat
capability, these have a fuel capacity reduced by 685 liters. The
F-2Bs will be used for conversion and proficiency training,
replacing Mitsubishi T-2s.
|
Video of the Mitsubishi F-2
close-support fighter |
|
|