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General characteristics F7F-1 | |||
Primary function | Fighter | ||
Contractor | Grumman Aircraft Engineering Corporation | ||
Power plant | Two Pratt&Whitney R-2800-22W engines | ||
Thrust | 2x 2,072 HP | 2x 1,545 kW | |
Wingspan | 51.5 ft | 15.7 m | |
Length | 45.4 ft | 13.85 m | |
Height | 16.6 ft | 5.06 m | |
Wingarea | 455 sq ft | 42.27 sq m | |
Weight | empty | 15,957 lb | 7,238 kg |
max. | 23,656 lb | 10,730 kg | |
Max. speed | 427 mph | 687 km/h | |
Ceiling | 36,090 ft | 11,000 m | |
Max. range | 1,790 miles | 2,880 km | |
Armament | 4x 20 mm cannon, 4x 12.7 mm machine gun 300 rounds each), 2x 454 kg bombs or 6x rockets. Alternative under fuselage 1x 21inch torpedo. | ||
First flight | December, 1943 | ||
Crew | One | ||
Date deployed | 1944 | ||
Number built | 250 |
Jirka Wagner
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