The KAI T-50 Golden Eagle is a series of South Korean supersonic advanced trainers and light combat aircraft designed and produced by Korea Aerospace Industries (KAI) together with Lockheed Martin. It is the first indigenous supersonic aircraft of South Korea and one of the few supersonic trainers in the world.

Korea Aerospace Industries
Korea, South
1900 to: Present
US$21 million (2008)
Honeywell H-764
1x General Electric F404-102
17,700 pound-force
Max Cruise Speed:
992 knots
1,837 Km/h
Approach Speed (Vref):
130 knots
Travel range:
999 Nautical Miles
1,850 Kilometers
Fuel Economy:
Service Ceiling:
48,000 feet
Rate of Climb:
39000 feet / minute
198.12metre / second
Take Off Distance:
Landing Distance:
Max Take Off Weight:
12,300 Kg
27,117 lbs
Max Landing Weight:
10,300 Kg
22,707 lbs
Max Payload:
5,830 Kg
12,853 lbs
Fuel Tank Capacity:
730 gallon
2,763 litre
Baggage Volume:
Seats - Economy / General:
2 seats
Seats - Business Class:
Seats - First Class:
Cabin Height:
Cabin Width:
Cabin Length:
Exterior Length:
13.14 metre - 43.11 feet
Tail height:
4.94 metre - 16.21 feet
Fuselage Diameter:
1 metre - 3.28 feet
Wing Span / Rotor Diameter:
9.45 metre - 31.00 feet
Wing Tips:
No Winglets

The KAI T-50 program was initially planned to develop an original South Korean trainer aircraft capable of supersonic flight, to train and equip pilots for the General Dynamics KF-16 and McDonnell Douglas F-15K, and to replace previous Northrop T-38 and Cessna A-37 trainers in service with the Republic of Korea Air Force (ROKAF). Generally, the T-50 family of aircraft is almost the same as the KF-16 in the configuration.

In February 2000, the aircraft was officially named as the T-50 Golden Eagle. The final assembly of the first T-50 started from January 15 to September 14, 2011. In August 2002, the T-50 conducted its maiden flight. An initial operational assessment took place from July 28 to August 14, 2003. KAI is currently working with Lockheed Martin for an international joint marketing program of the T-50. In December 2003, the ROKAF placed a production contract for twenty-five aircraft, expected to be delivered from 2005 to 2009.

The T-50 Golden Eagle is equipped with digital fly-by-wire controls and hands-on throttle-and-stick. The cockpit of the T-50 includes two multifunction displays by Honeywell, instrumentation displays, and a head-up display from BAE Systems. Lockheed Martin developed the full authority digital flight control system and avionics. The flight equipment incorporates a navigation/attack system, a Honeywell H-764G embedded global positioning/inertial navigation system, and an HG9550 radar altimeter, Collins Aerospace VIR-130A/instrument landing system, and ARN-153V advanced digital TACAN receiver. The cockpit is equipped with an Onboard Oxygen Generating System (OBOGS) and ejection seats from Martin-Baker.

The aircraft has an exterior length of 13.14 meters, a height of 4.94 meters, and a fuselage diameter of 1 meter. It is equipped with retractable tricycle undercarriage from Messier Dowty. The wheelbase is 5.2 meters.

General Electric F404-102 turbofan engine powers the T-50. The engine has a maximum power of 17,700 lbf. The T-50 has a maximum cruise speed of 992 knots and a travel range of 999 nautical miles. The service ceiling is 48,000 feet and the rate of climb is 39,000 feet per minute.

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