he Grumman F4F Wildcat is an American carrierbased fighter aircraft that entered service in 1940 with the United States Navy, and the British Royal Navy where it was initially known as the Martlet. First used by the British in the North Atlantic, the Wildcat was the only effective fighter available to the United States Navy and Marine Corps in the Pacific Theater during the early part of the Second World War. The disappointing Brewster Buffalo was withdrawn in favor of the Wildcat and replaced as aircraft became available.
With a top speed of 318 mph (512 km/h), the Wildcat was outperformed by the faster (331 mph (533 km/h)), more maneuverable, and longerranged Mitsubishi A6M Zero. US Navy pilots, including John "Jimmy" Thach, a pioneer of fighter tactics to deal with the A6M Zero, were greatly dissatisfied with the Wildcat's inferior performance against the Zero in the battles of the Coral Sea and Midway. The Wildcat has a claimed air combat killtoloss ratio of 5.9:1 in 1942 and 6.9:1 for the entire war.
Lessons learned from the Wildcat were later applied to the faster F6F Hellcat. While the Wildcat had better range and maneuverability at low speed. the Hellcat could rely on superior power and high speed performance to outperform the Zero. The Wildcat continued to be built throughout the remainder of the war to serve on escort carriers, where the larger and much heavier Hellcat could not be used.
The Wildcat was generally outperformed by the Mitsubishi Zero, its major opponent in the early part of the Pacific Theater but held its own partly because, with relatively heavy armor and selfsealing fuel tanks, the Grumman airframe could survive far more damage than its lightweight, unarmored Japanese rival. Many U.S. Navy fighter pilots were saved by the Wildcat's ZB homing device, which allowed them to find their carriers in poor visibility, provided they could get within the 30 mi (48 km) range of the homing beacon. (However, the Zed Baker was wildly inconsistent in practice, especially during the Battle of Midway, when an entire squadron of Wildcats crashed in the sea after failing to locate their carriers).
In the hands of an expert pilot with a tactical advantage, the Wildcat could prove a difficult opponent even against the formidable Zero. After analyzing Fleet Air Tactical Unit Intelligence Bureau reports describing the new carrier fighter, USN Commander "Jimmy" Thach devised a defensive tactic that allowed Wildcat formations to act in a coordinated maneuver to counter a diving attack, called the "Thach Weave". The most widely employed tactic during the Guadalcanal Campaign was highaltitude ambush, where hitandrun maneuvers were executed using altitude advantage. This was possible due to an early warning system composed of Coastwatchers and radar. On rare occasions, when Wildcats were unable to gain altitude in time, they would suffer many losses. On 2 October 1942, a Japanese air raid from Rabaul was not detected in time and the Cactus Air Force lost six Wildcats to only one Zero destroyed. During the most intense initial phase of the Guadalcanal Campaign, between 1 August and 15 November, combat records indicate that US lost 115 Wildcats and Japanese lost 106 Zeros to all causes; the Japanese lost many more pilots compared to the US.
Thach was greatly dissatisfied and a vocal critic of the Wildcat's performance during the war (as were many US carrier pilots), stating in his Midway action report;
It is indeed surprising that any of our pilots returned alive. Any success our fighter pilots may have had against the Japanese Zero fighter is not due to the performance of the airplane we fly but is the result of the comparatively poor marksmanship of the Japanese, stupid mistakes made by a few of their pilots and superior marksmanship and team work of some of our pilots. The F4F airplane is pitifully inferior in climb, maneuverability and speed.
General characteristics
Crew: 1
Length: 28 ft 9 in (8.76 m)
Wingspan: 38 ft 0 in (11.58 m)
Height: 11 ft 10 in (3.61 m)
Wing area: 260 sq ft (24 m2)
Airfoil: root: NACA 23015; tip: NACA 23009
Empty weight: 4,907 lb (2,226 kg)
Gross weight: 7,423 lb (3,367 kg)
Powerplant: 1 × Pratt & Whitney R183076 14cylinder aircooled radial piston engine, 1,200 hp (890 kW)
Propellers: 3bladed constantspeed propeller
Performance
Maximum speed: 331 mph (533 km/h, 288 kn)
Range: 845 mi (1,360 km, 734 nmi)
Service ceiling: 39,500 ft (12,000 m)
Rate of climb: 2,303 ft/min (11.70 m/s)
Wing loading: 28.5 lb/sq ft (139 kg/m2)
Power/mass: 0.282 kW/kg (0.172 hp/lb)
Armament
Guns: 4 × 0.50 in (12.7 mm) AN/M2 Browning machine guns with 450 rounds per gun
Bombs: 2 × 100 lb (45.4 kg) bombs and/or 2 × 58 US gal (48 imp gal; 220 l) drop tanks
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