Comparison of Dornier Alpha Jet and North American T-2 Buckeye [S]ave
| Attribute |  Dornier Alpha Jet × |  North American T-2 Buckeye × |
|---|---|---|
| General | ||
| Manufacturer | Dornier GmbH | North American Aviation NAA |
| Model | Dornier Alpha Jet | North American T-2 Buckeye |
| Country | Germany | United States |
| Manufactured from (year) | 1973 | 1958 |
| Manufactured to (year) | 1991 | 1970 |
| Type | Military Aircraft | Military Trainers |
| Icao | AJET | T2 |
| Performance | ||
| Engine | 2x 2 × SNECMA Turbomeca Larzac 04-C6 | 2x General Electric J85-GE-4 |
| Power, lbf (lbf) | 3,000 | 2,950 |
| Max cruise speed (km/h) | 1,000 | 839 |
| Approach speed (km/h) | 167 | - |
| Travel range (km) | 2,945 | 1,683 |
| Fuel economy (km/l) | 1.678 | - |
| Service ceiling (m) | 15,240 | 12,314 |
| Rate of climb (m/sec) | 60.96 | 31.5 |
| Take off distance (m) | 410 | - |
| Landing distance (m) | 610 | - |
| Weights | ||
| Max take off weight (kg) | 8,000 | 5,978 |
| Max payload (kg) | 2,500 | 300 |
| Fuel tank capacity (l) | 1,900 | 2,616 |
| Dimensions | ||
| Seats | 2 | 2 |
| Exterior length (m) | 13.23 | 11.8 |
| Tail height (m) | 4.19 | 4.5 |
| Fuselage diameter (m) | - | 1.2 |
| Wing span (m) | 9.11 | 11.6 |
| Wing tips | No Winglets | No Winglets |
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