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Grumman F8F Bearcat

F8F Bearcat
F8F Bearcat (flying).jpg
Role Fighter aircraft
National origin United States
Manufacturer Grumman
First flight 21 August 1944
Introduction 1945
Retired 1963 VNAF
Status Retired
Primary users United States Navy
United States Marine Corps
French Air Force
Royal Thai Air Force
Number built 1,265

The Grumman F8F Bearcat is an American single-engine carrier-based fighter aircraft introduced in late World War II. It went on to serve into the mid-20th century in the United States Navy, the United States Marine Corps, and the air forces of other nations. It would be Grumman Aircraft's final piston engined fighter aircraft. Modified versions have broken speed records for piston-engined aircraft, and are popular among warbird owners.

The Bearcat concept began during a meeting between Battle of Midway veteran F4F Wildcat pilots and Grumman Vice President Jake Swirbul at Pearl Harbor on 23 June 1942. At the meeting, Lieutenant Commander Jimmie Thach emphasized one of the most important requirements in a good fighter plane was "climb rate".

Climb performance is strongly related to the power-to-weight ratio, and is maximized by wrapping the smallest and lightest possible airframe around the most powerful available engine. Another goal was that the G-58 (Grumman's design designation for the aircraft) should be able to operate from escort carriers, which were then limited to the obsolescent F4F Wildcat as the Grumman F6F Hellcat was too large and heavy. A small, lightweight aircraft would make this possible. After intensively analyzing carrier warfare in the Pacific Theater of Operations for a year and a half, Grumman began development of the G-58 Bearcat in late 1943.

There is considerable debate among sources as to whether or not the Focke-Wulf Fw 190 influenced the design of the G-58. It is known that test pilots from Grumman examined and flew a captured Fw 190 in England in early 1943, and the G-58 has a number of design notes in common with the Fw 190 that the Hellcat did not, especially in the cowling and landing gear arrangements. However, no definitive evidence has been presented that these tests had a direct input to the G-58 design.


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