យន្តហោះធុន Chengdu J-20 មានសមត្ថភាពខ្ពស់ជាង ទំនើបជាង F-22 ដោយសារ ការស្ថាបនាយន្តហោះ Chengdu J-20 គឺ បន្ទាប់ពីការសិក្សាទៅលើ F-22 និង F-35 របស់សហរដ្ឋអាមេរិក។ វាមានទំហំធំជាង វែងជាង អាវុធទំនើបជាង ព្រមទាំងដោះស្រាយរាល់បញ្ហាដែល F-22 មានកន្លងមក។ ទ័ពអាកាសចិន បានតម្លើងតួរលេខនៃការផលិតពី ២៨ គ្រឿង ឡើងដល់ ៥០ គ្រឿងនៅឆ្នាំ ២០២០ ។
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Role | Stealth air superiority fighter |
National origin | China |
Manufacturer | Chengdu Aerospace Corporation |
First flight | 11 January 2011; 9 years ago |
Introduction | 10 March 2017 |
Status | In service |
Primary user | People's Liberation Army Air Force |
Produced | 2009–present |
Number built | 50 as of 2019 |
Program cost | US$4.4 billion |
Unit cost | • US$100–$110 million[8] (LRIP estimate as of 2018) |
• US$30–$50 million[9][10] (Flyaway cost estimate as of 2017) | |
Developed from | J-XX |
General characteristics | Armament |
Crew: one (pilot) | Internal weapon bays |
Length: 20.4 m (66.8 ft) | PL-10 short range AAM (30 Km) |
Wingspan: 13.5 m (44.2 ft) | PL-12 Medium Range AAM (70 Km) |
Wing area: 78 m2 (840 sq ft) | PL-15 BVR long range AAM (150 Km) |
Empty weight: 19,391 kg (42,750 lb) | PL-21 Long Range AAM |
Gross weight: 32,092 kg (70,750 lb) | LS-6 Precision-guided bomb |
Max takeoff weight: 37,013 kg (81,600[135] lb) | External hardpoints |
Fuel capacity: 11,340 kg (25,000 lb) internally | 4× under-wing pylon capable of carrying drop tanks. |
Powerplant: 2 × WS-10B or AL-31FM2 afterburning turbofan, 140 or 145 kN (31,000 or 33,000 lbf) with afterburner | Avionics |
Powerplant: 2 × Shenyang WS-15 (in development[6]) afterburning turbofan, 180 kN (40,000 lbf) with afterburner | Type 1475 (KLJ-5) active electronically scanned array |
Performance | EOTS-86 electro-optical targeting system (EOTS) |
Maximum speed: Mach 2[137][138][139] | EORD-31 infrared search and track |
Range: 6,000 km (3,700 mi, 3,200 nmi) | Distributed aperture system |
Combat range: 2,000 km (1,200 mi, 1,100 nmi) | |
Service ceiling: 20,000 m (66,000 ft) | |
g limits: +9/-3 | |
Rate of climb: 304[140] m/s (59,800 ft/min) | |
Wing loading: 340 kg/m2 (69 lb/sq ft) | |
Thrust/weight: 0.92 (1.12 with loaded weight and 50% fuel) with AL-31FM2 (estimated) |
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