| Blue Angels F11F Tiger 1957 |
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The Tiger single-seat fighter flew for the first time in prototype form on 30 July 1954 - less than 15 months after receipt of a letter of intent from the US Navy. The production version was the F11F-1. A small number of pre-production aircraft, each with a Wright J65-W-6 turbojet engine with afterburner, were followed by 39 production aircraft (ordered with J65-W-4 afterburning engines), two of which were modified to F11F-1F standard with 66.72kN General Electric J79-GE-7 afterburning engines. One of the F11F-1Fs attained a speed of 1,963km/h and set a short-lived height record on 18 April 1958 of 23,449m. |
A further contract for J65-W-18-engined Tigers placed for the US Navy brought the total number of F11F-1s built to about 200, but these were gradually phased out of first-line service from 1959. Those which remained in second-line service when the tri-service designations became rationalised in 1962 were redesignated F-11A. |
| Specification |   |
| CREW | 1 | |
| ENGINE | 1 x Wright J-65-W-6, 33.8kN | |
| WEIGHTS | ||
| Take-off weight | 6290-8380 kg | 13867 - 18475 lb |
| DIMENSIONS | ||
| Wingspan | 9.7 m | 31 ft 10 in |
| Length | 12.5 m | 41 ft 0 in |
| Height | 3.9 m | 12 ft 10 in |
| Wing area | 23.2 m2 | 249.72 sq ft |
| PERFORMANCE | ||
| Max. speed | 1430 km/h | 889 mph |
| Ceiling | 16700 m | 54800 ft |
| Range w/max.fuel | 1000 km | 621 miles |
| ARMAMENT | 4 x 20mm cannon, missiles | |
| 3-View |   |
![]() | A three-view drawing of F11F-1 Tiger (768 x 576) |
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