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The F-100 was designed originally as a higher performance follow-on to the F-86 air superiority fighter. Adapted as a fighter bomber, the F-100 would be supplanted by the Mach 2 class F-105 Thunderchief for strike missions over North Vietnam. The F-100 flew extensively over South Vietnam as the Air Force's primary close air support jet until replaced by the more efficient subsonic A-7 Corsair II The F-100 also served in several NATO air forces and with other US allies. In its later life, it was often referred to as "the Hun," a shortened version of "one hundred."
– Design & Development
– Variants
– Operational History
Type: Fighter-bomber Crew: 1 Manufacturer: North American Aviation Models: see variants Number built: 2,294 Primary Users: United States Air Force France, Denmark, Turkey, Taiwan |
Maiden flight: May 25, 1953 Service Delivery: Sept. 27, 1954 Retired (USAF): 1970 Retired (US ANG): 1979 Retired (Turkey): 1982 |
Specifications: F-100D Super Sabre
Powerplant: Model: Pratt & Whitney J57-P-21/21A Type: After-burning Turbojet Number: One Dry Thrust: 10,200 lb W. Afterburner: 16,000 lb Dimensions: Length: 50 ft (15.2 m) Wingspan: 38 ft 9 in (11.81 m) Height: 16 ft 2¾ in (4.95 m) Wing area: 400 ft² (37 m²) Wing loading: 72.1 lb/ft² (352 kg/m²) Thrust/weight: 0.55 Lift-to-drag ratio: 13.9 |
Weights: Empty: 21,000 lb (9,500 kg) Loaded: 28,847 lb (13,085 kg) Max takeoff: 34,832 lb (15,800 kg)
Performance: Armament: 4× 20 mm M39 cannon
Bombload: |
Sources:
Wikipedia: F-100 Super Sabre
WARBIRDS RESOURCE GROUP > VIETNAM > F-100 SUPER SABRE > PREVIOUS PAGE