J-31 (Jianjiji-31 Fighter aircraft 31)
Preliminary | 2015 Estimate | |
---|---|---|
Crew | one (pilot) | one (pilot) |
Length | 16 m (52 ft 6 in) 17.5 Meters (56.75 Feet) | 16.9 m (55 ft 5 in) |
Wing span | 10 m (32 ft 10 in) 13.1 Meters (42.5 Feet) | 11.5 m (37 ft 9 in) |
Canard span | none | |
Height | 5.35 Meters (17.4 Feet) | 4.8 m (15 ft 9 in) |
Wing area | 40 m2 (430 sq ft) | 40 m2 (430 sq ft) |
Empty weight | 17 Tons | 17,600 kg (38,801 lb) |
Loaded Weight? | 25 Tons | 28 tons [2016] |
T-O weight (normal) | ||
Fuel reserve, spec. weight | ||
Max landing weight, kg | ||
Max payload, kg | 8,000 kg | 8,000 kg |
Engines | 2 × Klimov RD-93 afterburning turbofans 196 kN (44,000 lbf) with afterburner |
84 kN (19,000 lbf) thrust each 100 kN (22,000 lbf) thrust each |
Thrust/weight | ~1 | |
Maximum speed, At altitude | Mach 1.8 (2,200 km/h) Mach 2.0 (1,500 mph, 2,400 km/h) ?? | 2,205 km/h (1,369 mph; 1,190 kn) Mach 1.8 |
Maximum speed, Supercruise Speed | ||
Service Ceiling | 16000 meters 20000 Meters (65,000 Feet) ??? | |
Combat Radius | 1200 km 2000 Kilometers (1200 Miles) ??? | 1,200 km (777 mi; 675 nmi) 1,250 km [2016] |
Ferry Range | 5500 Kilometers (3400 Miles) | 4,000 km (2,485 mi; 2,160 nmi) |
Max flight range with internal fuel reserve | ||
Max flight range with one in-flight refuelling | ||
Max T-O run at normal T-O weight (afterburner) | ||
Max landing run at normal landing weight | ||
Load factor limit, g | ||
Armament | the weapon-bay volume and Stores bays in four zones
2016 | |
Service Life | 30 years |
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