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The North American YF-93A, developed from the F-86 Sabre and originally designated F-86C, eventually became the third design in the penetration fighter competition with the McDonnell XF-88 and Lockheed XF-90. The YF-93A was a bigger, bulkier Sabre: the nose inlet of the F-86 design was replaced with side-mounted inlets and the fuselage was widened to house a 12835kg thrust Pratt & Whitney turbojet. The result was a larger, heavier machine with longer range and greater load-carrying capacity than the Sabre. On 9 June 1948, the USAF ordered 118 F-93s, but the
order was cancelled a year later. The YF-93A lost its second chance to attain production status when it emerged a poor third in the penetration fighter contest which, as it turned out, did not result in any production contract anyway.
The first of the two YF-93As, also known as the company NA-157, was first flown on 24 January 1950. The two machines underwent various modifications during evaluation, including changes in the shape of their lateral air inlets. After the USAF was no longer a potential buyer, the two airframes were turned over to the National Advisory Committee for Aeronautics (NACA), where they were employed in various tests until eventually being retired and scrapped.
 | A three-view drawing (1280 x 822) |
| MODEL | YF-93A |
| WEIGHTS |
| Take-off weight | 12025 kg | 26511 lb |
| Empty weight | 16360 kg | 36068 lb |
| DIMENSIONS |
| Wingspan | 11.81 m | 38 ft 9 in |
| Length | 13.44 m | 44 ft 1 in |
| Height | 4.78 m | 15 ft 8 in |
| Wing area | 28.43 m2 | 306.02 sq ft |
| PERFORMANCE |
| Max. speed | 1140 km/h | 708 mph |
| Ceiling | 14265 m | 46800 ft |
| John Heron, thudjock(@)btinternet.com, 12.06.2008 12835kgs (28,000lbs) from a 1950s P&W powerplant? More like 2835 kgs from the J48. Also the weights quoted are inaccurate where the TO weight is shown to be much less than the quoted empty weight. The corrrect weights should be about 14,500lb empty and 21,000lb normal operating |
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