| Attribute | McDonnell Douglas F-15 Eagle × | McDonnell Douglas F-4 Phantom II × |
|---|---|---|
| General | ||
| Manufacturer | McDonnell Douglas | McDonnell Douglas |
| Model | McDonnell Douglas F-15 Eagle | McDonnell Douglas F-4 Phantom II |
| Country | United States | United States |
| Manufactured from (year) | 1972 | 1958 |
| Manufactured to (year) | - | 1981 |
| Type | Fighter Jets | Fighter Jets |
| Icao | F15 | F4 |
| Performance | ||
| Engine | 2x Pratt & Whitney F100-PW-220 | 2x 2 × General Electric J79-GE-17A Turbojets |
| Power, lbf (lbf) | 23,770 | 17,900 |
| Avionics | F15 HUD, APG-63 and 70 pulse-Doppler radar | - |
| Max cruise speed (km/h) | 3,019 | 2,371 |
| Approach speed (km/h) | 463 | - |
| Travel range (km) | 5,556 | 2,815 |
| Fuel economy (km/l) | - | 0.205 |
| Service ceiling (m) | 19,812 | 18,898 |
| Rate of climb (m/sec) | 254 | 209.8 |
| Take off distance (m) | 275 | 1,370 |
| Landing distance (m) | 1,100 | 1,120 |
| Weights | ||
| Max take off weight (kg) | 30,844 | 28,030 |
| Max landing weight (kg) | 20,185 | 16,706 |
| Max payload (kg) | 10,659 | 8,500 |
| Fuel tank capacity (l) | 16,448 | 12,624 |
| Dimensions | ||
| Seats | 1 | 2 |
| Exterior length (m) | 19.43 | 19.2 |
| Tail height (m) | 5.64 | 5 |
| Wing span (m) | 13.06 | 11.7 |
| Wing tips | No Winglets | No Winglets |