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McDonnell F-101 Voodoo

| General characteristics | |||
| Primary function | Fighter | ||
| Contractor | McDonnell Aircraft Company, later a division of McDonnell-Douglas, St. Louis | ||
| Power plant | Two Pratt & Whitney J-57-P-55 turbojets with afterburner | ||
| Thrust with afterburner | 2x 16,900 lb | 2x 75.18 kN | |
| Wingspan | 39.6 ft | 12.08 m | |
| Length | 67.4 ft | 20.54 m | |
| Height | 18 ft | 5.49 m | |
| Max. speed | 1,134 mph | 1,825 km/h | |
| Initial climb rate | 49,200 ft/s | 14,996 m/min. | |
| Ceiling | 52,000 ft | 15,850 m | |
| Range | normal | 1,522 miles | 2,450 km |
| max. | 1,930 miles | 3,106 km | |
| Max. takeoff weight | 52,404 lb | 23,770 kg | |
| Armament | 20mm cannons; 6x AIM in weapons bay (usually 3x GAR-1 (AIM-4) semiactive radar guided missiles and 3x GAR-2 (AIM-4B) infra-red guided). Later version two unguided nuclear AIR-2A Genie missiles on external points. | ||
| Number built | 480 | ||
Jirka Wagner
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Last updated 01.10.2008