Comparison of Lockheed P-80 Shooting Star and Lockheed T-33 Shooting Star [S]ave
| Attribute |  Lockheed T-33 Shooting Star × |  Lockheed P-80 Shooting Star × |
|---|---|---|
| General | ||
| Manufacturer | Lockheed Martin Aeronautics | Lockheed Martin Aeronautics |
| Model | Lockheed T-33 Shooting Star | Lockheed P-80 Shooting Star |
| Country | United States | United States |
| Manufactured from (year) | 1948 | 1945 |
| Manufactured to (year) | 1959 | 1950 |
| Type | Military Trainers | Fighter Jets |
| Icao | T33 | P80 |
| Performance | ||
| Engine | 1x Allison J33-A-35 | 1x Allison J33-A-35 |
| Power, lbf (lbf) | 5,400 | 4,600 |
| Max cruise speed (km/h) | 963 | 956 |
| Approach speed (km/h) | 193 | - |
| Travel range (km) | 2,052 | 2,222 |
| Service ceiling (m) | 14,630 | 14,265 |
| Rate of climb (m/sec) | 24.74 | 34.9 |
| Take off distance (m) | 1,706 | - |
| Landing distance (m) | 1,417 | - |
| Weights | ||
| Max take off weight (kg) | 6,832 | 7,257 |
| Max landing weight (kg) | 5,475 | 6,350 |
| Max payload (kg) | 700 | 1,000 |
| Fuel tank capacity (l) | 3,078 | 3,350 |
| Dimensions | ||
| Seats | 2 | 1 |
| Exterior length (m) | 11.51 | 10.5 |
| Tail height (m) | 3.56 | 3.45 |
| Fuselage diameter (m) | 1.1 | 1 |
| Wing span (m) | 11.85 | 11.83 |
| Wing tips | No Winglets | No Winglets |
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