Notes: This was
one of Japan’s first post-war fighter designs, being first produced in 1967.
It is a combat version of the T-2 trainer, with the rear seat replaced by
additional fuel and avionics, a gun and hardpoints added, and the nose filled
with radar and more avionics. It
bears a marked (though coincidental) resemblance to the Jaguar, and it is often
mistaken for the Jaguar at air shows.
The F-1’s primary job in the JASDAF is antishipping work, though most of
the air-to-ground ordnance and gear of Japan may be used by the F-1. The F-1 was
retired in 2006 in favor of the F-2, with 77 being built. During the 1990s, 70
of the F-1s were given a Service Life Extension Program (SLEP) to increase their
lifetimes until sufficient quantities of the F-2 were in service.
The wings of the
F-1 are small for the aircraft size, with a wingspan of only 7.88 meters, and
this leads to the relatively poor maneuverability of the F-1. The two wingtip
hardpoints may only carry heat-seeking air-to-air missiles or the Sidearm
antiradiation missile; extra fuel tanks may be carried on the centerline and
inboard wing hardpoints. The F-1 is powered by two Ishikawa-Harima TF40-801A
afterburning turbofan engines, delivering 5100 pounds thrust dry each or 8000
pounds thrust each in afterburner. These are licensed copies of the Rolls Royce
Turbomeca Adour engine. The radar is likewise a licensed copy of the US
AN/AWG-12 radar fitted to the F-4E Phantom II, and is designated the J/AWG-12.
Twilight 2000
Notes: The main limitations on the use of the F-1 during the Twilight War were
its short range and the inability to refuel from US or South Korean tanker
aircraft.
|
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
$11,482,589 |
JP5 |
2.72 tons |
13.7 tons |
1 |
15 |
Radar (100 km) |
Enclosed |
|
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Armor |
|
2904 |
807 (130) |
NA 218
6/3 60/30 |
3848 |
2072 |
15240 |
FF4 CF4
RF4 W4
T3 |
|
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
RWR, Flare/Chaff Dispensers (30/20), HUD, Track While Scan, Laser
Designator (20 km), INS |
810/540m Hardened Runway |
+2 |
20mm M61A1 Vulcan Autocannon, 7 Hardpoints |
750x20mm |
Mitsubishi F-2
Notes: In the
late 1980s, Japan was looking for an aircraft to replace its aging and outmoded
F-1 strike fighters. To this end,
they designed the FS-X, based on an enlarged and modernized F-16C Block 40
airframe; after more modernization and development, this became the F-2.
Compared to the F-16C, the F-2 is a much more capable aircraft, with
air-to-air capability nearly on par with the F-15 and an air-to-ground
capability similar to the F/A-18. The F-2 is nicknamed by its pilots the Viper
Zero, from the popular nickname of the F-16 and the Mitsubishi A6M Zero of World
War 2 fame. Compared to the F-16C Block 40, the F-2 has much larger wings, much
larger tail surfaces, and a somewhat larger fuselage. To keep weight down, much
of the wing structure is made from graphite-epoxy composites. 98 were built, but
some were prototypes, some test aircraft, and a few were destroyed in accidents.
Production ended in 2011.
Active chaff was
developed for the F-2 similar to that used in the Eurofighter; this chaff is one
level better in fighting lock-on and guidance attempts.
In addition, the composite wing structure gives the F-2 some minor
stealth benefits; radar has a -2 penalty when trying to detect the F-2, and
attempts to guide radar-homing missiles to the F-2 also have a -2 penalty. The
pilot has three LCD MFDs in the cockpit to control most of the functions of the
aircraft. The F-2 actually has five
hardpoints under each wing, to accommodate different loads, but only a maximum
of four hardpoints under each wing may be employed at any one time, due to space
requirements. The two wingtip hardpoints may only be loaded with air-to-air
missiles, antiradiation missiles, or electronics pods or flare and chaff pods.
Two of the hardpoints on each wing and the centerline hardpoint are plumbed for
carrying extra fuel tanks. The F-2 is powered by a General Electric F110-IHI-129
afterburning turbofan engine, developing 17000 pounds of thrust dry or 29500
pounds of thrust in afterburner. The radar is a powerful AESA radar, the
J/APG-2. The radios have a Link-16 and datalink compatibility and can talk to
ground troops, ships, or other aircraft and receive information from AWACS-type
aircraft and other tactical aircraft.
Twilight 2000
Notes: These aircraft were standouts in the Twilight War, both over Korea and in
defense of Japan.
|
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
$22,057,355 |
JP5 |
11.82 tons |
22.09 tons |
1 |
21 |
Radar (222 km), Image Intensification (40 km) |
Shielded |
|
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Armor |
|
3998 |
1110 (115) |
NA 300
10/6 100/60 |
4637 |
3452 |
18000 |
FF6 CF6
RF6 W5
T5 |
|
Combat Equipment |
Minimum Landing/Takeoff Zone |
RF |
Armament |
Ammo |
|
All-Weather Flight, RWR, IFF, Flare/Chaff Dispensers (50/30), ECM 2, EW
Suite, Auto Track, HUD, IR Uncage, Track While Scan, Multitarget (2),
Target ID, Laser Designator (30 km), INS |
800/530m Hardened Runway |
+4 |
20mm M61A2 Vulcan, 11 Hardpoints |
750x20mm |