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Mitsubishi T-2

Military Aircraft

The Mitsubishi T-2 was a twin-engine supersonic jet trainer designed and built by Mitsubishi for the Japan Air Self-Defense Force, and the first Japanese-developed aircraft to break the sound barrier. The Fuji T-1 could not prepare pilots for Mach 2 fighters, so Japan chose its own design over licence-building the Jaguar or the T-38, selecting Mitsubishi in September 1967. The first XT-2 prototype flew on 20 July 1971, and the type entered service in 1975. It flew with the Blue Impulse aerobatic team and as an aggressor trainer, and served as conversion trainer for its strike derivative, the F-1. Ninety were built, the last in 1988, and all were withdrawn by 2006.

Facts
Year
1971 1
Engine Class
Jet 1
Status
Out of production 1
Units Built
90 1
Top Speed (km/h)
1700 1
Mass (kg)
6197 1
Maximum Mass (kg)
12,800 1
Comparison
Body Style
Aircraft (no road body style) 1
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Exemplifies

Aviation, Modes
Source Mitsubishi T-2 (Wikipedia)

Of Make

Source Mitsubishi T-2 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Mitsubishi T-2 (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
designed and produced by the Japanese aerospace firm Mitsubishi

Originated In

Also in Geography Atlas: where this subject originated.

Source Mitsubishi T-2 (Wikipedia)Lead
Quote, Lead
was a supersonic jet trainer aircraft designed and produced by the Japanese aerospace firm Mitsubishi
Sources
1. Mitsubishi T-2 (Wikipedia)
  • Lead
    was a supersonic jet trainer aircraft designed and produced by the Japanese aerospace firm Mitsubishi
  • Lead, first flight
    On 20 July 1971, the first XT-2 prototype performed its maiden flight.
  • Production
    During 1988, the last T-2 rolled off the assembly line.
  • Production, total
    A total of 90 production T-2s were constructed
  • Specifications, maximum speed
    Maximum speed: 1,700 km/h (1,100 mph, 920 kn) at 10,975 m (36,007 ft)
  • Specifications, empty weight
    Empty weight: 6,197 kg (13,662 lb)
  • Specifications, max takeoff weight
    Max takeoff weight: 12,800 kg (28,219 lb)
  • Specifications, powerplant
    2 × Ishikawa-Harima TF40-801A afterburning turbofan
  • Lead, manufacturer
    designed and produced by the Japanese aerospace firm Mitsubishi
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