The F-1 was retired from service in 2006. It was superseded with F-2A, which is derived from Lockheed Martin's F-16 Fighter Jet.
Mitsubishi F-1 fighter design
The exterior design of the F-1 is similar to the Sepecat Jaguar fighter jet. The aircraft was designed by modifying its forerunner Mitsubishi T-2 advance trainer jet, which is built based on the Sepecat Jaguar.
The design was modified to include two wing pylons and a fuselage pylon, replace the rear cockpit with an avionics bay and an unglazed access hatch in place of a glass canopy.
F-1 development
"The F-1 was the first indigenous fighter aircraft built post-World War II."
In 1972, the JASDF announced its plan to build the strike fighter model (F-1) from the T-2 trainer jet. The development contract was awarded in 1973. Two T-2s were acquired by the JASDF to transform them into F-1 prototypes. The aircraft was developed to supersede the fleet of F-86 Sabres.
The F-1's maiden flight took place in June 1975 and the aircraft entered service in April 1978. The JASDAF initially planned to build 160 units; however, budget cuts reduced the numbers to 77. Final delivery of the F-1 took place in March 1987.
The JASDF launched a service life extension programme (SLEP) in 1990s to increase the lifespan of an airframe from 3,500 hours to 4,000 hours. As part of the SLEP, 70 F-1s were overhauled between 1991 and 1993 by incorporating a modern fire control system, a robust canopy and an XGCS homing bomb.Features
The F-1 aircraft has two drop tanks of 830l capacity, each under its centreline pylon and wings. A tubular antenna is fitted at the top of the tail fin and J / AWG-12 radar. It can attack from relatively short range and can be utilised in interception missions.
Cockpit
The all-digital cockpit is enclosed with a glass canopy to accommodate one flight crew. It is equipped with head up display (HUD) and J / ASQ-1 fire control system (FCS) developed by Mitsubishi Electric.
"The F-1 supersedes the F-86 Sabres."
A radar warning receiver, a J / ASN-1 inertial navigation system, a J / APR-3 radar homing warning system, a J / APN-44 radar altimeter system, a J / A24G-3 air data computer, a strike camera system and imaging infra-red seeker system form part of the cockpit.
Armaments
The F-1 is armed with a 20mm JM61A1 Vulcan 6 barrelled Gatling cannon in the front fuselage section to fire munitions at the rate of 6,000 rounds per minute. The aircraft has seven hardpoints: four under the wings, one under the centreline pylon station and two wing tip missile rails. It can carry up to 2,721kg payload.
The aircraft can accommodate Mitsubishi AAM-1 and two AIM-9L Sidewinder air-to-air missiles, two Mitsubishi ASM-1 anti-ship missiles, JLAU-3A 70mm rocket pods, RL-7 70mm rockets, RL-4 125mm rockets and LAU-69 rocket pods.
It can also carry Mk-82 and M117 bombs weighing 226kg and 340kg, respectively. Other payloads incorporated in the aircraft are air-to-ground missiles and infra-red guided versions of MK82 and M117.
Ishikawa-Harima engines
"The F-1 can climb at a rate of 118m per second."
The F-1 is powered by two Ishikawa-Harima TF40-801A turbofan engines, each rated at 22.8kN of dry thrust. The thrust afterburner of the engine is 35.6kN.
Designed and manufactured by IHI Corporation of Japan, the TF40-801A is a licence-built version of Adour Mk801 which is a variant of the Turbomeca Adour engine.
The dry weight of the engine is 3,300kg.
F-1 performance
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