Here a links for their specs
2 hp = 1 pound of thrust
Corsair
Wingspan
40 ft. 10 in.
Overall Length
33 ft. 8 in.
Height
14 ft. 9 in.
Empty Weight
9,206 lbs.
Gross Weight
14,670 lbs.
Fuel Capacity
534 gal.
Oil Capacity
20 gal.
Engine
Pratt & Whitney R-2800-18W 18 cylinder, twin row, air-cooled radial, 2,450 hp with water injection
Propeller
Hamilton Standard 4-blade, 13 ft. 2 in. diameter
Maximum Speed, Sea Level
446 mph
Initial Rate-of-Climb
3,870 ft./min.
Cruise Speed, Sea Level
215 mph
Range at Cruise Speed
1,015 miles
Service Ceiling
41,500 ft.
Crew
1
Armament
Six .50 cal machine guns
Bomb Load
up to 4,000 lb on centerline and pylon racks
Zero
Specifications (A6M5):
Engine: One 1130-hp Nakajima NK1C Sakae 21 radial piston engine.
Weight: Empty 4175 lbs., Max Takeoff 6504 lbs.
Wing Span: 36ft. 1in.
Length: 29ft. 9in.
Height: 11ft. 5.75in.
Maximum Speed: 346mph
Ceiling: 35,100 ft.
Range: 1118 miles with internal fuel.
Armament: Two 20-mm cannon and two 7.7-mm machine guns.
The poll
 | Which would win? |
| F-4U Corsair | |
| A6M Zero | |
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