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T-4

T-4

Training Jets
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Basic Information
Name
T-4
Designation
T-4
Alternate Designation
T-4 Blue Impulse (JASDF aerobatic display team)
Equipment Type
Training Jets
Manufacturer
Kawasaki Heavy Industries (KHI), Mitsubishi Heavy Industries
Date of Introduction
1988
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.

Air & Air Defense Specifications
Crew 2
Max Speed 1038.0 km/h
Range 1667.0 km
Service Ceiling 15240 m
Wingspan 9.90 m
Overview (Deagel)
Group Training Jets
Status Active
Also Known As T-4 Blue Impulse (JASDF aerobatic display team)
Origin Japan
Contractors Kawasaki Heavy Industries (KHI)*, Mitsubishi Heavy Industries
Initial Operational Capability (IOC) 1988
First Flight July 29, 1985
Total Production 180
Specifications (Deagel)
Crew 2
Number of Engines 2
Area — Wing Area 21 square meter
Dimensions — Height 4.6 meter
Dimensions — Length 13 meter
Dimensions — Wingspan 9.9 meter
Mass — Empty Weight 3,790 kilogram
Mass — Max Takeoff Thrust 7,360 pound
Mass — Max Takeoff Weight 7,500 kilogram
Mass — Payload 2,000 kilogram
Performance — Ceiling 50,000 foot
Performance — Max Range 1,667 kilometer
Speed — Climb Rate 10,240 fpm
Speed — Cruise Speed 797 kph
Speed — Top Speed at High Altitude 1,038 kph
Speed — Top Speed at Sea Level 1,038 kph
Gear (Deagel)
Item 1 Fighter Aircraft Engines: F-3-30 (2)
Details
Country of Origin Japan
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
13 m
Width
9.9 m
Height
4.6 m
Weight
7500 kg
Operators (1)
Japan
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