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At a glance
Measured figures
estimated · Length
Single source22.28 m (73 ft 1 in)[source]
Length
Single sourceConfiguration
| Specification | Shenyang J-15 | Sukhoi Su-75 Checkmate |
|---|---|---|
| Type | Carrier-based multirole fighter[source] | Stealth multirole fighter[source] |
| National origin | China[source] | Russia[source] |
| Manufacturer | Shenyang Aircraft Corporation[source] | Sukhoi Komsomolsk-on-Amur Aircraft Plant[source] |
| Status | In service / In production[source] | Under development |
17.7 m (58 ft 1 in)[source]
Empty; estimated · Empty weight
Single sourceGross; estimated · Gross weight
Single sourceMaximum take-off; estimated · Max takeoff weight
Single source17,500 kg (38,581 lb)[source]
27,000 kg (59,525 lb)[source]
33,000 kg (72,753 lb)[source]
Maximum take-off; Max takeoff weight
Single source26,000 kg (57,320 lb)[source]
Maximum; estimated · Maximum speed
Single source2,300 km/h (1,400 mph, 1,200 kn)[source]
Maximum; at sea level
Single sourceMaximum; Mach 1.8 at high altitude Mach 1.06
Single sourceMach 1.8, 1,910 km/h (1,030 kn; 1,190 mph) at high altitude Mach 1.06, 1,300 km/h (702 kn; 808 mph) at sea level[source]
estimated · Combat range
Single source1,270 km (790 mi, 690 nmi)[source]
estimated · 2 × Saturn AL-31 or WS-10B afterburning turbofans with afterburner
Single source2 × Saturn AL-31 or WS-10B afterburning turbofans, 122.6–135 kN (27,600–30,300 lbf) with afterburner[source]
1 × NPO Saturn AL-51F-1 (derivative) afterburning turbofan thrust dry
Single sourcewith afterburner
Single source1 × NPO Saturn AL-51F-1 (derivative) afterburning turbofan , 107.9 kN (24,300 lbf) thrust dry, 161.9 kN (36,400 lbf) with afterburner[source]
estimated · Wing area
Single source67.84 m 2 (730.2 sq ft)[source]
Hardpoints: 5 internal, 6 external with a capacity of maximum payload, with provisions to carry combinations of
Single sourceHardpoints: 5 internal, 6 external with a capacity of 7,400 kilograms (16,300 lb) maximum payload, with provisions to carry combinations of:[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary user | People's Liberation Army Naval Air Force[source] | — |
|---|
| Number built | 116+[source] | — |
|---|
| Manufactured | 2006–present[source] | — |
|---|
| Introduction date | J-15: December 2013 J-15S: July 2022 J-15T/J-15D: October 2024[source] | — |
|---|
| First flight | J-15: 31 August 2009 J-15S: 3 November 2012 J-15T: July 2016 J-15D: October 2016[source] | — |
|---|
| Developed from | T-10K Shenyang J-11B[source] | — |
|---|
| Fuel capacity | 9,800 kg (21,600 lb) internal[source] | — |
|---|
| g limits | +8 g[source] | +8.0[source] |
|---|
| Thrust/weight | 0.93 with AL-31 (1.01-1.07 with WS-10B)[source] | 1.0:1[source] |
|---|
| Hardpoints | Munitions on twelve external hardpoints with a capacity of 6,500 kg, including:[source] | 5 internal, 6 external with a capacity of 7,400 kilograms (16,300 lb) maximum payload, with provisions to carry combinations of: Missiles: 3 x BVRAAM and 2 x SRAAM stored in the internal weapons bay, 6 × external, 2 × R-77 , 3 × R-73 , 2 × Kh-35 E anti-ship missiles[source] |
|---|
| Designer | — | Sukhoi Design Bureau[source] |
|---|
| Missiles | — | 3 x BVRAAM and 2 x SRAAM stored in the internal weapons bay, 6 × external, 2 × R-77 , 3 × R-73 , 2 × Kh-35 E anti-ship missiles[source] |
|---|