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Old 08-24-2010, 08:38 PM   #7
pollyjolly123
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1/72 Corgi Vought F4U-1 Corsair, United States Marine Corps




Quoting Wikipedia:
"The performance of the Corsair was impressive. The F4U-1 was considerably faster than the F6F Hellcat and only 13 mph (21 km/h) slower than the P-47 Thunderbolt,[27][28][29] both of the two other fighters also being powered by the R-2800. But while the P-47 achieved its highest speed at 30,020 feet (9,150 m) with the help of an intercooled turbosupercharger,[30] the F4U-1 reached its maximum speed at 19,900 ft (6,100 m),[31] and used a mechanically supercharged engine.[32]
Carrier qualification trials on the escort carrier USS Sangamon, on 25 September 1942, caused the U.S. Navy to release the type to the United States Marine Corps.[33] Early Navy pilots spoke disparagingly of the F4U as the "hog", "hosenose" or "bent wing widow-maker".[34] After all, the U.S. Navy still had the Grumman F6F Hellcat, which did not have the performance of the F4U but was a far better deck landing aircraft. The Marines needed a better fighter than the F4F Wildcat. For them it was not as important the F4U could be recovered aboard a carrier, as they usually flew from land bases. Growing pains aside, Marine Corps squadrons readily took to the radical new fighter.[35]"



Once again quoting wikipedia:
"F4U-1 (Corsair Mk I Fleet Air Arm): The first production version of the Corsair with the original cockpit seat height and "bird cage" canopy.[N 5] The differences over the XF4U-1 were as follows:
Six .50 in (12.7 mm) Browning AN/M2 machine guns were fitted in the outer wing panels, displacing fuel tanks.
An enlarged 237 gal (897 l) fuel tank was fitted ahead of the cockpit, in place of the fuselage armament. The cockpit was moved back by 32 in (810 mm).
The fuselage was lengthened from 31 feet 11 inches (9.73 m) to 33 feet 4 inches (10.16 m).
The more powerful R-2800-8 Double Wasp was fitted.
150 pounds (68 kg) of armor plate was fitted to the cockpit and a 1.5 in (38 mm) bullet-resistant glass screen was fitted behind the curved windscreen.
IFF transponder equipment was fitted.
Curved transparent panels were incorporated into the fuselage behind the pilot's headrest.
The flaps were changed from deflector type to NACA slotted.
The span of the ailerons was increased while that of the flaps was decreased.
One 62 gal (234 l) non-self-sealing auxiliary fuel cell was installed in each wing leading edge, just outboard of the guns.
A land-based version for the USMC, without the folding wing capability, was built by Goodyear under the designation FG-1. In Fleet Air Arm service the F4U-1 was given the name Corsair Mk I.[92] Vought also built a single F4U-1 two-seat trainer; the Navy showed no interest.[93]"


Notice the uncharacteristic "birdcage" canopy on the F4U-1, something not seen on the later models.
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