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 |