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Lockheed F-104 Starfighter
| General characteristics F-104A | |||
| Primary function | Fighter | ||
| Contractor | Lockheed Aircraft Corporation | ||
| Power plant | One General Electric J79-GE-3A/3B turbojet engine with afterburner | ||
| Speed | max. | 1,047 mph | 1,669 km/h |
| min. | 195 mph | 314 km/h | |
| Initial climb rate | 1,006 ft/s | 307 m/s | |
| Ceiling | 64,830 ft | 19,760 m | |
| Range | normal | 730 miles | 1,174 km |
| maximum | 1,400 miles | 2,250 km | |
| Wingspan | 21 ft 9 in | 6.6 m | |
| Length | 54 ft 8 in | 16.7 m | |
| Height | 13 ft 5 in | 4 m | |
| Weight | empty | 13,184 lb | 5,980 kg |
| max. takeoff | 25,840 lb | 11,720 kg | |
| Crew | One | ||
| Armament | One 20mm M61A1 cannon (725 rounds); 2x AIM-9B Sidewinder on wingtips; 4,000 lb of bombs under the wings. | ||
Jirka Wagner
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Last updated 13.11.2012