Mitsubishi Heavy Industries
T-2
The Mitsubishi T‑2 was Japan’s first domestically designed supersonic jet trainer, conceived by Mitsubishi Heavy Industries in the early 1970s to replace the aging piston‑engine trainers of the Japan Air Self‑Defense Force. Development began in 1969, and the prototype first flew on 14 July 1971; after a rigorous flight‑test programme the aircraft entered operational service in 1975. Powered by two afterburning turbofan engines, the T‑2 could reach Mach 1.5 and featured a swept‑wing layout, a glass‑cockpit later upgraded to digital displays, and an ejection seat for each crew member. Its airframe incorporated lightweight aluminum alloys and featured hardpoints for weapons training, allowing pilots to practice air‑to‑air and air‑to‑ground tactics. Over 200 units were produced, and the type remained the backbone of advanced jet training in Japan for more than three decades, later giving rise to the more modern Kawasaki T‑4. The T‑2’s significance lies in establishing an indigenous high‑performance jet programme, proving Japan’s capability to design, produce, and sustain supersonic aircraft, and providing a bridge to later fighter development such as the F‑1 and subsequent multirole jets. Today, the T‑2 remains a celebrated example of Japanese aerospace engineering and a benchmark for future trainers.
Classification
Dimensions
- Length
- 703 inch
- Mass
- 21274 pound
Performance
- Service Ceiling
- 50025 foot
- Range
- 1550 nautical mile
Production & History
- Units Produced
- 90
- First Flight
- 1971
Design & Classification
- Primary Use
- Country of Origin
- Manufacturer
- Mitsubishi Heavy Industries
- Developer
- Mitsubishi Heavy Industries
- Military Designation
- T-2
- Engine
- RT.172 Adour
- Operator
-
Japan Air Self-Defense Force
- Wikidata ID
- Q1153321