Mitsubishi T-2

ICAO aircraft code T2
Country Japan

The Mitsubishi T-2 was a supersonic jet trainer aircraft used by the Japan Air Self-Defense Force.

Specifications

Full description

Similar aircraft

Mitsubishi T-2 specifications

General

ICAO aircraft code
T2
Manufacturer
Mitsubishi Heavy Industries
Manufactured
1971 - 1988
Country
Japan

Aircraft performance

Avionics:
Mitsubishi Electric J/AWG-11, French Thomson-CSF HUD, Lear-Siegler 501OBL AHRS
Engine:
2x Ishikawa-Harima TF40-801A
Turbofan
Power:
7,140 pound-force
Max Cruise Speed:
920 Kts
1,704 Km/h
Travel range:
1,550 Nm
2,871 Kilometers
Service Ceiling:
50,000 feet
Rate of Climb:
35000 feet / minute
177.80meter / second

Weight & dimensions

Max Take Off Weight:
12,800 Kg
28,219 lbs
Max Payload:
2,700 Kg
5,952 lbs
Fuel Tank Capacity:
1,010 gallon
3,823 liter

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

About the Mitsubishi T-2

The Mitsubishi T-2 was a supersonic jet trainer aircraft used by the Japan Air Self-Defense Force. Introduced in 1975, it was the first Japanese-designed aircraft to break the sound barrier. It was the basis of the Mitsubishi F-1 military aircraft. All T-2s were retired by 2006.

Other Mitsubishi Heavy Industries aircraft

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