| Attribute | Northrop F-5 Tiger × | Dornier Alpha Jet × |
|---|---|---|
| General | ||
| Manufacturer | Northrop Grumman | Dornier GmbH |
| Model | Northrop F-5 Tiger | Dornier Alpha Jet |
| Country | United States | Germany |
| Manufactured from (year) | 1962 | 1973 |
| Manufactured to (year) | 1987 | 1991 |
| Type | Fighter Jets | Military Aircraft |
| Icao | F5 | AJET |
| Performance | ||
| Engine | 2x General Electric J85-GE-21B turbojet | 2x 2 × SNECMA Turbomeca Larzac 04-C6 |
| Power, lbf (lbf) | 5,000 | 3,000 |
| Avionics | Emerson Electric AN/APQ-153/157/159, AN/APG-69 | - |
| Max cruise speed (km/h) | 1,737 | 1,000 |
| Approach speed (km/h) | 230 | 167 |
| Travel range (km) | 3,723 | 2,945 |
| Fuel economy (km/l) | 1.614 | 1.678 |
| Service ceiling (m) | 15,789 | 15,240 |
| Rate of climb (m/sec) | 175.26 | 60.96 |
| Take off distance (m) | 884 | 410 |
| Landing distance (m) | 762 | 610 |
| Weights | ||
| Max take off weight (kg) | 11,192 | 8,000 |
| Max payload (kg) | 3,200 | 2,500 |
| Fuel tank capacity (l) | 2,650 | 1,900 |
| Dimensions | ||
| Seats | 1 | 2 |
| Exterior length (m) | 14.45 | 13.23 |
| Tail height (m) | 4.06 | 4.19 |
| Fuselage diameter (m) | 1 | - |
| Wing span (m) | 8.13 | 9.11 |
| Wing tips | No Winglets | No Winglets |