Mitsubishi F-1

F-1
F-1 at Misawa Base (1994)
General information
TypeAttack aircraft
National originJapan
ManufacturerMitsubishi Heavy Industries
Primary userJapan Air Self Defense Force
Number built77[1]
History
Manufactured1975–1987[1]
Introduction dateApril 1978
First flight3 June 1975[1]
RetiredMarch 2006
Developed fromMitsubishi T-2

The Mitsubishi F-1 is a single-seat twin-engine supersonic strike aircraft designed and produced by the Japanese conglomerate Mitsubishi Heavy Industries. It was Japan's first domestically developed supersonic combat aircraft.[1]

Developed during the early 1970s, the F-1 is essentially a combat-orientated derivative of the Mitsubishi T-2 trainer aircraft, which was also procured for the Japan Air Self-Defense Force (JASDF); accordingly, it was initially referred to as the FS-T2kai prior to being redesignated as F-1. Key modifications included the removal of the second seat in the cockpit for an avionics bay, airframe strengthening, and the installation of additional hardpoints. While the F-1 was not a highly manoeuvrable aircraft, it was intended for advanced avionics and intense training to be decisive factors in the event of live combat. The F-1 was primarily oriented towards the ground attack and anti-shipping missions, in which it was viewed as being a suitable counter to Soviet warships. Secondarily, it was also intended to function as an air defence fighter.

The F-1 performed its maiden flight on 3 June 1975, and entered service with the JASDF just over two years later. No other operators emerged for the type; production was terminated in 1987 after 77 aircraft were completed. Despite its prospective replacement by a more capable aircraft being openly discussed by the mid-1980s, the majority of the fleet underwent a service life extension programme (SLEP) during the 1990s and remained in active service until 2006, at which point the last F-1s were withdrawn in favour of the more capable F-2.

Design and development

F-1 in flight. Note the anti-ship missiles being carried underwing
A pair of F-1s in formation flight, 2002

In the mid 1960s, the Japan Air Self-Defense Force (JASDF) commenced studies into an advanced jet trainer which could also be modified to serve in the ground attack and anti-shipping roles. After considering the license production of the several overseas aircraft, including the American Northrop T-38 Talon and the Anglo/French SEPECAT Jaguar, Japan decided to develop its own trainer, the supersonic Mitsubishi T-2, which made its maiden flight on 20 July 1971.[2] During 1972, the JASDF announced its intention to procure the F-1 strike fighter derivative to succeed its aging North American F-86 Sabre fleet.[3]

Cost over-runs on the T-2 program led to the proposed single seat attack version almost being abandoned, but the cancellation of the Kawasaki P-XL, the planned replacement for Japan's Kawasaki P-2J maritime patrol aircraft released funds while simultaneously raising the importance of keeping Japan's aviation industry engaged upon sufficient work, thus contracts were awarded for the development of the attack version as the FS-T2kai in 1973.[4][5] A major driving force for a new combat aircraft was the desire for a capable close air support platform which could be deployed against a potential amphibious attack upon Japan by the Soviet Union, although the F-1 would not be specifically designed for this mission.[6]

The new aircraft was a minimum change derivative of the T-2, with the rear cockpit being converted to an avionics bay by removing the rear seat, and replacing the canopy with a simple unglazed access hatch.[7][1] Two additional hardpoints were fitted under the wing to allow carriage of a heavier weapon load, and the avionics were improved,[8] which included the addition of a Ferranti-supplied inertial navigation system, Thomson-CSF-supplied head-up display, J/ASQ-1 bombing computer, and J/AWG-12 radar set (the latter being similar to the AN/AWG-12 sets fitted in British Royal Air Force F-4M Phantom fighter jets).[9][1] This set provides ranging information. Aside from the avionics changes, deletion of the rear seat, and new one-piece canopy, the only other major change from the T-2 was the strengthening of the airframe to enable it to carry a larger weapons load than the T-2. The F-1 is fitted with an internally mounted 20 mm JM61A1 Vulcan cannon with 750 rounds of ammunition. The aircraft also had a total of seven external hardpoints for the carriage of a wide variety of stores (missiles, gun pods, etc.). The fuselage hardpoint and inboard pair of underwing hardpoints are plumbed for external fuel tanks to increase the aircraft's range.[1]

The primary weapon of the F-1 is the ASM-1 (and the newer ASM-2) long-range anti-ship missile. This weapon is roughly in the class of the American AGM-84 Harpoon or French AM.39 Exocet. Other weapons carried include the all-aspect short-range heat-seeking AIM-9 Sidewinder air-to-air missile for air-to-air combat. Typically, this weapon was carried on the wingtip rails, but it could also be carried on the outboard underwing hardpoints for the F-1's secondary air defense role.[3] Other air-to-ground weapons carried include rocket pods (JLAU-3/A) of 70 mm (2.75 in) size as well as bombs of 227 kg (500 lb) and 340 kg (750 lb) in size (Mk82 and M117 respectively). In addition, the Mk-82 and M117 bombs can be fitted with infrared guidance kits, turning them into precision-guided weapons that home in on heat radiation emitted from seaborne targets such as ships or other ground-based targets. When fitted with this kit, the bomb becomes known as GCS-1.

While the JASDAF had initially planned to procure 160 F-1s, this was reduced down to 77 aircraft, primarily as a result of budget cuts. Production of the type was terminated in 1987.[1][3]

Operational history

During late 1977, the F-1 entered operational service with the Japan Air Self-Defense Force (JASDF).[1] Deliveries of the type continued until March 1987. A total of 77 F-1s would see operational use.[1]

Operationally, substantial focus was placed upon the F-1's role as a maritime defence platform and the prospective use of its sizable anti-ship missiles to strike enemy warships.[10] Additionally, the F-1 held a secondary role to patrol Japanese airspace, despite its survivability in air-to-air combat being a persistent cause for concern due to the aircraft not being particularly manoeuvrable or aerodynamically advanced. As an aerial interceptor, the F-1 was heavily reliant upon the capabilities of its avionics, such as its search and detection radar, being superior to that of its potential opponents; it was also believed that superior discipline, intensive training, and more advanced air-to-air missiles would be decisive factors in such an engagement.[11]

During the 1990s, 70 F-1s were recipients of a service life extension programme (SLEP), which increased the operational life of their airframes from 3,500 hours to 4,000 hours.[3]

By the mid-1980s, Japanese defence planners were already considering the F-1's prospective replacement by a more capable successor aircraft.[12][1] The F-1 was ultimately replaced by the F-2 (Japan/U.S. developed, based on the F-16C/D Agile Falcon), as well as upgraded F-4EJ Kai Phantom IIs.[13] The last six active F-1s, based at Tsuiki in Fukuoka Prefecture, were retired on 9 March 2006,[14] having reached the 4,000 hour limit of their airframes.

Variants

FS-T2-Kai

Prototypes, two built.

Mitsubishi F-1

Single-seat close air support, ground-attack and anti-ship fighter aircraft. 77 built.[3]

Operators

 Japan

Survivors / Aircraft on display

F-1 on display at Fuchū Air Base, Tokyo
F-1 at Tsuiki Air Field, Fukuoka Prefecture, Japan

Specifications (F-1)

Cockpit of an F-1
Canopies of a T-2 (above) and F-1 (below)

Data from Mitsubishi's Sabre Successor[16]

General characteristics

  • Crew: 1
  • Length: 17.86 m (58 ft 7 in)
  • Wingspan: 7.88 m (25 ft 10 in)
  • Height: 4.48 m (14 ft 8 in)
  • Wing area: 21.2 m2 (228 sq ft)
  • Empty weight: 6,358 kg (14,017 lb)
  • Max takeoff weight: 13,674 kg (30,146 lb)
  • Powerplant: 2 × Ishikawa-Harima TF40-801A afterburning turbofan engines, 22.8 kN (5,100 lbf) thrust each dry, 35.6 kN (8,000 lbf) with afterburner

Performance

  • Maximum speed: 1,700 km/h (1,100 mph, 920 kn) at 11,000 m (36,000 ft) (clean)
  • Combat range: 556 km (345 mi, 300 nmi) High-Low-High profile with two ASM-1 missiles and one 830 L (220 US gal; 180 imp gal) drop tank
  • Ferry range: 2,870 km (1,780 mi, 1,550 nmi) (max external fuel)
  • Service ceiling: 15,240 m (50,000 ft) [17]
  • Time to altitude: 11,000 m (36,000 ft) in two minutes
  • Wing loading: 645 kg/m2 (132 lb/sq ft)

Armament

See also

Related development

Aircraft of comparable role, configuration, and era

References

Citations

  1. ^ a b c d e f g h i j k Air Force Magazine 1990, p. 75.
  2. ^ Lake 1994, p. 145.
  3. ^ a b c d e "Mitsubishi F-1 Fighter Aircraft". airforce-technology.com. Retrieved 6 April 2026.
  4. ^ Lake 1995, pp. 52–53.
  5. ^ Sekigawa 1980, pp. 117–120.
  6. ^ Drohan 2015, p. 114.
  7. ^ Lake 1995, p. 53.
  8. ^ Sekigawa 1980, pp. 120–121.
  9. ^ Lake 1995, p. 68.
  10. ^ Drohan 2015, pp. 114-115.
  11. ^ Drohan 2015, p. 115.
  12. ^ Drohan 2015, pp. 114-117.
  13. ^ "Lockheed Martin continues work for Japan's F-2 fighter". Defense Daily. 23 April 1998. Archived from the original on 24 September 2015. Retrieved 28 May 2015.
  14. ^ https://www.milavia.net/aircraft/f-1/f-1.htm
  15. ^ a b c d e f g h i j k l m n o p q r Thompson, Paul J-HangarSpace - Where Are They Now? Retrieved September 16, 2016
  16. ^ Sekigawa 1980, p. 130.
  17. ^ Michell 1994, p. 128.

Bibliography

  • "Fighters: issues 7-12". Air Force Magazine. Vol. 73. Air Force Association. 1990.
  • Drohan, Thomas A. (2015). American-Japanese Security Agreements, Past and Present. McFarland. ISBN 9-78147-660775-7.
  • Eden, Paul, ed. (2004). The Encyclopedia of Modern Military Aircraft. London, UK: Amber Books. ISBN 1-904687-84-9.{{cite book}}: CS1 maint: ref duplicates default (link)
  • Lake, Jon (Winter 1995). "Mitsubishi F‑1: Ship‑killing Samurai". World Air Power Journal. Vol. 23. London, UK: Aerospace Publishing. pp. 50–71. ISBN 978-1-874023-64-7. ISSN 0959-7050.
  • Lake, Jon (Autumn 1994). "Mitsubishi T‑2: Supersonic Samurai". World Air Power Journal. Vol. 18. pp. 136–147. ISBN 1-874023-45-X. ISSN 0959-7050.
  • Michell, Simon (1994). Simon Michell (ed.). Jane's Civil and Military Aircraft Upgrades 1994–95. Coulsdon, UK: Jane's Information Group. ISBN 0-7106-1208-7.
  • Sekigawa, Eiichiro (March 1980). "Mitsubishi's Sabre Successor". Air International. Vol. 18, no. 3. Bromley, UK: Fine Scroll. pp. 117–121, 130–131. ISSN 0306-5634.