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General Info

North American
F-100 Super Sabre

Role Fighter Fighter-bomber
Manufacturer North American Aviation
First flight 25 May 1953
Introduction 27 September 1954
Retired 1979, United States Air National Guard; 1988, Republic of China Air Force
Primary users United States Air Force Turkish Air Force Republic of China Air Force French Air Force
Produced 1953–1959
Number built 2,294
Developed from North American F-86 Sabre
Developed into North American F-107

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History North American Aviation
F-100 Super Sabrejet
The F-100 was envisioned during late 1940s as a higher-performance successor to the F-86 Sabre air superiority fighter.[4] Initially referred to as the Sabre 45, it was delivered as an unsolicited proposal to the USAF in January 1951, leading to two prototypes being ordered one year later following modifications. The first YF-100A performed its maiden flight on 25 May 1953, seven months ahead of schedule. Flight testing demonstrated both the F-100's promising performance and several deficiencies, which included its tendency of yaw instability and inertia coupling that led to numerous fatal accidents. On 27 September 1954, the F-100A officially entered USAF service, however, as a result of six major accidents occurred by 10 November 1954, the type was grounded while investigations and remedial work were conducted. The F-100 returned to flight in February 1955.

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North American

North American F-100 Super Sabre

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General characteristics

  • Crew: 1
  • Length: 50 ft (15 m)
  • Wingspan: 38 ft 9 in (11.81 m)
  • Height: 16 ft 2.75 in (4.9467 m)
  • Wing area: 400 sq ft (37 m2)
  • Aspect ratio: 3.76
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Powerplant

  • Drag area: 5.0 sq ft (0.46 m2)
  • Empty weight: 21,000 lb (9,525 kg)
  • Gross weight: 28,847 lb (13,085 kg)
  • Max takeoff weight: (15,800 kg)
  • Powerplant: 1 × Pratt & Whitney J57-P-21/21A afterburning turbojet engine, 10,200 lbf (45 kN) thrust dry, 16,000 lbf (71 kN) with afterburner
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Specifications

  • Maximum speed:  (1,487 km/h, 803 kn)
  • Maximum speed: Mach 1.4
  • Range: 1,995 mi (3,211 km, 1,734 nmi)
  • Service ceiling: 50,000 ft (15,000 m)
  • Rate of climb: 22,400 ft/min (114 m/s)
  • Lift-to-drag: 13.9
  • Wing loading: 72.1 lb/sq ft (352 kg/m2)
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Armament

Special Links North American F-100 Super Sabrejet

Links to Youtube & Others

On 27 September 1954, the F-100A officially entered USAF service with the 479th Fighter Wing, based at George AFB, California. By 10 November 1954, the F-100As suffered six major accidents

First Supersonic
 Fighter USAF

The North American F-100 Super Sabre is an American supersonic jet fighter aircraft designed and produced by North American Aviation.

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Youtube Link

F-86B 188 ordered as upgraded A-model with wider fuselage and larger tires but delivered as F-86A-5, North American model NA-152

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Aircrafttotal : Airforces

Read more in USAF /  USA Air Force

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