| Attribute | Grumman F11F Tiger × | Lockheed F-94 Starfire × |
|---|---|---|
| General | ||
| Manufacturer | Grumman | Lockheed Martin Aeronautics |
| Model | Grumman F11F Tiger | Lockheed F-94 Starfire |
| Country | United States | United States |
| Manufactured from (year) | 1954 | 1949 |
| Manufactured to (year) | 1959 | 1954 |
| Type | Fighter Jets | Fighter Jets |
| Icao | F11F | F94 |
| Performance | ||
| Engine | 1x Wright J65-W-18 afterburning turbojet | 1x Pratt & Whitney J48-P-5 |
| Power, lbf (lbf) | 10,500 | 8,750 |
| Avionics | AN/ARC-27A UHF COMMS, AN/ARA-25 UHF, AN/ARR-40 UHF, AN/ARN-14E VHF Nav etc. | AN/APG-40 radar |
| Max cruise speed (km/h) | 1,213 | 1,037 |
| Travel range (km) | 2,056 | 2,052 |
| Service ceiling (m) | 12,771 | 15,667 |
| Rate of climb (m/sec) | 82.8 | 40.54 |
| Weights | ||
| Max take off weight (kg) | 10,641 | 10,970 |
| Max landing weight (kg) | 9,541 | 8,300 |
| Max payload (kg) | 1,360 | 800 |
| Fuel tank capacity (l) | 3,872 | 5,777 |
| Dimensions | ||
| Seats | 1 | 2 |
| Exterior length (m) | 13.98 | 13.56 |
| Tail height (m) | 4.03 | 4.55 |
| Fuselage diameter (m) | 0.7 | 1.4 |
| Wing span (m) | 9.64 | 13.4 |
| Wing tips | No Winglets | No Winglets |