ACombat aircraft
KAI T-50 Golden Eagle
T-50: Advanced trainer jet TA-50: Lead-in fighter-trainer FA-50: Light combat aircraft FA-50 Block 20: Multirole light fighter
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
ACombat aircraft
T-50: Advanced trainer jet TA-50: Lead-in fighter-trainer FA-50: Light combat aircraft FA-50 Block 20: Multirole light fighter
At a glance
Measured figures
T-50 · Length
Single source13.14 m (43 ft 1 in)[source]
Length
Single sourceConfiguration
| Specification | KAI T-50 Golden Eagle | Sukhoi Su-33 |
|---|---|---|
| Type | T-50: Advanced trainer jet TA-50: Lead-in fighter-trainer FA-50: Light combat aircraft FA-50 Block 20: Multirole light fighter[source] | Carrier-based air superiority fighter with multirole capabilities[source] |
| National origin | South Korea[source] | Soviet Union Russia[source] |
| Manufacturer | Korea Aerospace Industries Lockheed Martin[source] | Sukhoi , Komsomolsk-on-Amur Aircraft Production Association[source] |
| Status | In service[source] |
21.19 m (69 ft 6 in)[source]
wing folded
Single source7.40 m (24 ft 3 in) wing folded[source]
T-50 · 1 × General Electric F404 -GE-102 afterburning turbofan engine (built under license by Samsung Techwin ) thrust dry
Single sourceT-50 · with afterburner
Single source1 × General Electric F404 -GE-102 afterburning turbofan engine (built under license by Samsung Techwin ), 53.07 kN (11,930 lbf) thrust dry, 78.7 kN (17,700 lbf) with afterburner[source]
2 × Saturn AL-31F3 afterburning turbofan engines thrust each dry
Single sourcewith afterburner
Single sourceT-50 · Hardpoints: Total of 7 with 4 underwing, 2 wingtip and one under fuselage; holding up to of payload
Single sourceHardpoints: Total of 7 with 4 underwing, 2 wingtip and one under fuselage; holding up to 5,400 kg (12,000 lb) of payload[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In service[source] |
| Primary users | Republic of Korea Air Force Iraqi Air Force Indonesian Air Force Royal Thai Air Force[source] | — |
|---|
| Number built | 200 (all models)[source] | 24 built total[source] |
|---|
| Manufactured | 2001–present[source] | 1987–1999[source] |
|---|
| Introduction date | 22 February 2005[source] | 31 August 1998 (official)[source] |
|---|
| First flight | 20 August 2002[source] | 17 August 1987 ( 1987-08-17 )[source] |
|---|
| Fuel capacity | 2,655 liters (701 U.S. gal) internal[source] | 9,500 kg (20,900 lb) internal[source] |
|---|
| Guns | 1× General Dynamics M197 20mm (0.787 in) 3-barrel rotary electric cannon, 205 rounds[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] |
|---|
| Hardpoints | Total of 7 with 4 underwing, 2 wingtip and one under fuselage; holding up to 5,400 kg (12,000 lb) of payload[source] | 12 × external hardpoints with a capacity of up to 6,500 kg (14,300 lb) of ordnance, with provisions to carry combinations of: Rockets: S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU Missiles: Air-to-air missiles : 8 × R-27 R/ER/T/ET 4 × R-73 E Anti-ship missiles : Kh-31 A Kh-41 Anti-radiation missiles : Kh-25 MP Kh-31 P Bombs: RBK-500 cluster bomb Up to 500 kg (1,100 lb) bombs[source] |
|---|
| g limits | + 8 − 3[source] | + 8[source] |
|---|
| Thrust/weight | 0.96[source] | 0.83[source] |
|---|
| Missiles | Air-to-air missiles: AIM-9L/M Sidewinder AIM-9X Sidewinder (Block 70) AIM-120 AMRAAM (Block 70) Air-to-ground missiles: AGM-65 Maverick[source] | Air-to-air missiles : 8 × R-27 R/ER/T/ET 4 × R-73 E Anti-ship missiles : Kh-31 A Kh-41 Anti-radiation missiles : Kh-25 MP Kh-31 P[source] |
|---|
| Air-to-air missiles | AIM-9L/M Sidewinder AIM-9X Sidewinder (Block 70) AIM-120 AMRAAM (Block 70)[source] | — |
|---|
| Air-to-ground missiles | AGM-65 Maverick[source] | — |
|---|
| Bombs | GBU-38 Joint Direct Attack Munition GBU-12 Paveway II KGGB Mark 82 bomb CBU-105 WCMD Sensor Fuzed Weapon CBU-58 SUU-20 Dispenser[source] | RBK-500 cluster bomb Up to 500 kg (1,100 lb) bombs[source] |
|---|
| Others | Sniper Advanced Targeting Pod[source] | — |
|---|
| Primary user | — | Russian Navy[source] |
|---|
| Developed from | — | Sukhoi Su-27[source] |
|---|
| Variant | — | Shenyang J-15[source] |
|---|
| Stall speed | — | 240 km/h (150 mph, 130 kn)[source] |
|---|
| Wing loading | — | 483 kg/m 2 (99 lb/sq ft)[source] |
|---|
| Landing speed | — | 240 km/h (150 mph; 130 kn)[source] |
|---|
| Rockets | — | S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU[source] |
|---|
Maximum take-off; Max takeoff weight
2 × Saturn AL-31F3 afterburning turbofan engines, 74.5 kN (16,700 lbf) thrust each dry, 125.5 kN (28,200 lbf) with afterburner[source]