Mitsubishi F-2A
Explore the Mitsubishi F-2A in side view and top view to compare its silhouette and proportions.
From Wikipedia
The Mitsubishi F-2 is a multirole fighter that was derived from the General Dynamics F-16 Fighting Falcon, and manufactured by Mitsubishi Heavy Industries and Lockheed Martin for the Japan Air Self-Defense Force, with a 60/40 split in manufacturing between Japan and the United States. The basis of the F-2's design is the F-16C Block 40. Production started in 1996 and the first aircraft entered service in 2000.
Summary of “Mitsubishi F-2” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
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Drawing of the Mitsubishi F-2A by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/F2/), CC BY 4.0Specifications
- Length
- 15.52 m50.9 ft
- Wingspan
- 11.12 m36.5 ft
- Max take-off weight
- 22.1 t48,700 lb
- Max speed
- 2,124 km/h1,320 mph
- Ceiling
- 18,000 m59,100 ft
- Engines
- 1 × General Electric F110-IHI-129 afterburning turbofan
- Power
- 76 kN (17,000 lbf) thrust dry, 131 kN (29,500 lbf) with afterburner
- First flight
- 1995
- In service
- 2000
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.