Mitsubishi F-1

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. 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programme (SLEP) during the 1990s and remained in active service until 2006, at which point the last F-1s were withdrawn in favour of the more capable F-2.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Mitsubishi Heavy Industries
- Category
- Attack aircraft
- First flight
- 1975-06-03
Specifications
- Cruise speed
- 920 kt
- Max speed
- 920 kt
- Range
- 300 nm
- Service ceiling
- 50,000 ft
- Rate of climb
- 3,000 ft/min
- Max takeoff weight
- 30,146 lb
- Empty weight
- 14,017 lb
- Fuel capacity
- 220 US gal
- Powerplant
- 2 × Ishikawa-Harima TF40-801A
- Engines
- 2
- Seats
- 1
- Length
- 58.6 ft
- Wingspan
- 25.8 ft
- Height
- 14.7 ft
- Number built
- 77
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.