page_title: North American YF-93
section_title: Specifications (YF-93A)
hierarchical_section_title: North American YF-93 / Specifications (YF-93A)
caption_attribution_description: English: Cut-away drawing of the North American YF-93A.
context_page_description: The North American YF-93 was an American fighter development of the F-86 Sabre that emerged as a radically different variant that received its own designation. Two were built and flown before the project was eventually canceled.
context_section_description: Data from The American Fighter
  General characteristics
  Crew: 1
  Length: 44 ft 1 in (13.44 m)
  Wingspan: 38 ft 9 in (11.81 m)
  Height: 15 ft 8 in (4.78 m)
  Wing area: 306 sq ft (28.4 m²)
  Empty weight: 14,035 lb (6,366 kg)
  Gross weight: 21,610 lb (9,802 kg)
  Max takeoff weight: 26,516 lb (12,027 kg)
  Powerplant: 1 × Pratt & Whitney J48-P-6 turbojet, 6,000 lbf (27 kN) thrust dry, 8,750 lbf (38.9 kN) with afterburner
  Performance
  Maximum speed: 708 mph (1,139 km/h, 615 kn) at sea level, 622 mph (1,001 km/h; 541 kn) at 35,000 ft (11,000 m)
  Cruise speed: 534 mph (859 km/h, 464 kn)
  Range: 1,967 mi (3,166 km, 1,709 nmi)
  Service ceiling: 46,800 ft (14,300 m)
  Rate of climb: 11,960 ft/min (60.8 m/s)
  Armament
  Guns: 6× 20mm M24 cannon (proposed, not fitted to the prototypes)
caption: Cut-away illustration of the YF-93A.
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