| Attribute | Shenyang J-15 × | McDonnell Douglas F-4 Phantom II × |
|---|---|---|
| General | ||
| Manufacturer | Shenyang | McDonnell Douglas |
| Model | Shenyang J-15 | McDonnell Douglas F-4 Phantom II |
| Country | China | United States |
| Manufactured from (year) | 2009 | 1958 |
| Manufactured to (year) | - | 1981 |
| Type | Fighter Jets | Fighter Jets |
| Icao | J15 | F4 |
| Performance | ||
| Engine | 2x Shenyang WS-10 | 2x 2 × General Electric J79-GE-17A Turbojets |
| Power, lbf (lbf) | 30,000 | 17,900 |
| Avionics | Shenyang Aircraft Corporation / MIL-STD-1553B | - |
| Max cruise speed (km/h) | 2,409 | 2,371 |
| Approach speed (km/h) | 241 | - |
| Travel range (km) | 3,519 | 2,815 |
| Fuel economy (km/l) | - | 0.205 |
| Service ceiling (m) | 20,117 | 18,898 |
| Rate of climb (m/sec) | 325.12 | 209.8 |
| Take off distance (m) | - | 1,370 |
| Landing distance (m) | - | 1,120 |
| Weights | ||
| Max take off weight (kg) | 33,000 | 28,030 |
| Max landing weight (kg) | 24,000 | 16,706 |
| Max payload (kg) | 15,000 | 8,500 |
| Fuel tank capacity (l) | 14,006 | 12,624 |
| Dimensions | ||
| Seats | 2 | 2 |
| Exterior length (m) | 21.9 | 19.2 |
| Tail height (m) | 5.92 | 5 |
| Fuselage diameter (m) | 1.8 | - |
| Wing span (m) | 14.7 | 11.7 |
| Wing tips | No Winglets | No Winglets |