F-CK-1A/B
| GENERAL DATA | |||
| Type |
Fighter
|
||
| Manufacturer(s) | Aerospace Industrial
Development Corporation |
||
| Prototype first flight | May 28, 1989 |
Introduction | January 1994 |
| Produced | 1990–2000 (A/B models) |
Number built | 103 + 10 prototypes (F-CK-1A) 27 + 1 prototype (F-CK-1B) |
| Status | In service |
Crew | 1, 2 (F-CK-1B) |
| Variants | |||
| F-CK-1A | Single-seater fighter, 3 prototypes and 103 standard aircraft. | ||
| F-CK-1B | Two-seater training fighter, 1 prototype and 27 standard aircraft. | ||
| F-CK-1C/D | Improvement of 127 A / B. | ||
| XT-5 Blue Magpie | Advanced training aircraft based on F-CK-1, to be built to 66 units by 2026. | ||
| DIMENSIONS (F-CK-1A) | |||
| Length | 14.48 m |
Empty Weight | 6500 kg |
| Wingspan | 9 m |
Loaded Weight | 9072 kg |
| Height | 4.42 m |
Max takeoff weight | 12247 kg |
| Wing area | 24.2 m² |
Wing loading | 504.9 kg/m² |
| ARMAMENT | |||
| Guns | 1× 20 mm (0.787 in) M61A1
6-barreled Gatling cannon |
Ammunition Carried |
515 |
| Other Armament | 9 hardpoints of 4080 kg of military
load |
||
| Missiles | 4× Sky Sword I, 4×
Sky Sword II
|
||
| Bombs | 2x Wan Chien air-to-ground cruise
missile |
||
| POWERPLANT | |||
| Engine | 2 ×
Honeywell/ITEC F125-70 Turbofan
|
||
| Dry thrust | 2722 kgp (27
kN) each |
Thrust with afterburner | 4309 kgp (42.1 kN) each |
| Thrust/weight | 1.01
|
Fuel Capacity | 2115 kg internally (F-CK-1A) 1884 kg internally (F-CK-1B) |
| PERFORMANCES | |||
| Maximum Speed | Mach 1.8
(2220 km/h) at altitude |
Stall Speed | 186
km/h |
| Range | 1100 km |
Service ceiling | 16800 |
| Sources | |||
| Wikipédia | aviationsmilitaires.net | ||
Drawings |
