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T-4  
Initial Operational Capability (IOC): 1988
Maiden Flight: 29 July 1985
Total Production: 180
Also Known As: T-4 Blue Impulse
Origin: Japan
Corporations: Kawasaki Heavy Industries (KHI)* and Mitsubishi Heavy Industries   (*) lead contractor
Parent System: T-4
Initial Operational Capability (IOC): 1988
Maiden Flight: 29 July 1985
Total Production: 180
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Description: The Kawasaki T-4 is an intermediate and advanced trainer similar to the European Alpha Jet designed to provide fighter aircraft training. The T-4 was developed by Kawasaki to meet the requirements of the Japan Air Self-Defense Force (JASDF) for a T-1 and T-33 training aircraft replacement in the 1980s. The first prototype flew on July 29, 1985. The JASDF took delivery of the first production T-4 aircraft in 1988. The JASDF requirement called for the production of approximately180-200 T-4s by 2000. Fuji and Mitsubishi were also involved in the airframe manufacturing.

The tandem twin-seat T-4 training aircraft is powered by two Ishikawajima-Harima (IHI) F3-IHI-30 turbofan engines each rated at 3,680-lb of thrust. The T-4 can achieve a top speed of 1,038 kph and has a maximum range of 1,200 kilometers or 1,600 kilometers with two droppable fuel tanks. The aircraft was designed to carry weaponry using underwing pylons. In addition to the training role, the T-4 can be serve as liaison aircraft. The JASDF also provided the T-4 to its aerobatic display team called the Blue Impulse.

T-4 Specifications

Crew: 2
Number of Engines: 2
Area
Wing Area: 21 square meter (226 square foot)
Dimensions
Height: 4.60 meter (15.1 foot)
Length: 13 meter (43 foot)
Wingspan: 9.94 meter (32.6 foot)
Performance
Ceiling: 50,000 foot (15,240 meter)
Max Range: 1,667 kilometer (900 nautical mile)
Speed
Climb Rate: 10,240 fpm (52 mps)
Cruise Speed: 797 kph (431 KTAS)
Top Speed at High Altitude: 1,038 kph (561 KTAS)
Top Speed at Sea Level: 1,038 kph (0.87 mach)
Weight
Empty Weight: 3,790 kilogram (8,355 pound)
Max Takeoff Thrust: 7,360 pound (3,338 kilogram)
Max Takeoff Weight: 7,500 kilogram (16,534 pound)
Payload: 2,000 kilogram (4,409 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Operators & Related Equipment


OperatorsItems
Japan180

Grand Total 1801
 
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