Posted on 10/21/2003 12:02:11 AM PDT by SAMWolf
Bump for a later read . . . have a blessed day!
Moving was successfully accomplished and with only minor injuries. However, I do not as yet have broadband access from my home. This is a bad thing.
Just lettin' you know I'm alive and more or less well :)
Oh my goodness Dark you should see my fabric closet! I am a quilter! Well I don't do much of it now.
I have so much fabric it's taking over my 4 room apt. Not LOL!!
Major Gregory "Pappy" Boyington
C.O. VMF-214, Black Sheep Squadron
"Just name a hero, and I'll prove he's a bum." - Pappy's self-assessment
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Air Power |
Originating in a 1938 Navy spec, when the need to replace the F2A and F4F could already be foreseen, the Vought Corsair was designed around an engine that also didn't exist yet: the Pratt & Whitney R-2800 Double Wasp, a monster 18 cylinder double radial, eventually capable of 2250 horsepower. (During the Corsair's development, corporate reorganizations brought the Vought company into Vought-Sikorsky and then Chance Vought, all part of United Aircraft, along with Pratt & Whitney and Hamilton Standard.)
The huge engine dictated much of the plane's design. Such a powerplant needed a comparably big propeller to absorb all that horsepower. Thus the 13' 4" diameter Hamilton Standard prop, the largest fitted to a fighter at that time. The Corsair's fuselage had to be high in the air, to give the prop clearance, But ordinary, straight wings at that height would have implied long (and weak) landing gear. The distinctive bent wings were developed to permit a reasonably short undercarriage.
The XF4U first flew in May 1940, and in October flew faster than 400 MPH, a record for a production fighter. A major re-design pushed the cockpit back 32 inches, which resulted in poor forward vision for the pilot, at least on take-off and landing. Development continued into 1942, when Vought delivered the first production F4U-1 to the Navy, which didn't like what it saw, especially when compared to the easier-handling, and very capable F6F Hellcat. The F4U had dangerous stall behavior, had tendency to yaw suddenly when landing, and, worst off all, bounced when it hit the deck. For use on carriers, these problems caused the Navy to insist that they be fixed, while it went ahead equipping with the Hellcat.
But the Marines, operating from land bases in the Solomons, needed capable new fighters to replace their aging F4F Wildcats. By late 1942, the first USMC squadron, VMF-124, took delivery of the Corsair F4U-1. In early 1943, they began to see combat, and were a huge success - with speed, maneuverability, firepower, and ability to absorb battle damage. By the summer of 1943, most of the Marine fighting squadrons had transitioned to the F4U-1, the first operational model, fitted with a distinctive "birdcage" canopy, as shown in the detail of a plane flown by Ed Olander (number 576). Boyington's squadron, VMF-214, switched over to Corsairs before they started their September 1943 combat tour.
The F4U is regarded by many as one of the greatest combat aircraft in history, and was in production for a longer period of time than any US fighter other than the F4 Phantom. As conceived it was intended to mount the most powerful engine, and biggest propeller, of any fighter in existence, and the prototype was the first US combat aircraft to exceed 400mph. However, early experience suggested that the design was in fact a disastrous failure, especially for carrier operations. The extraordinarily long nose interfered with visibility ahead in a way which particularly caused problems during landing and take-off. The undercarriage had a tendency to break, and the aircraft also had an inclination to bounce alarmingly on landing. As a result the US Navy at first rejected it for shipboard operation. Nonetheless the F4U was adopted by the Marine Corps and quickly demonstrated its effectiveness. Although its low rate-of-turn made it a very limited dogfighter its merits more than compensated for this and its other faults. Its great power, speed and rate of climb, its capacity to roll very rapidly, combined with a powerful armament - and large ammunition supply - and a quite exceptional resistance to battle damage, meant that in early 1943 ( in the Solomons) it quickly demonstrated its great superiority over the enemy fighters. By the end of hostilities in the Pacific War it had established an 11:1 "kill" ratio against Japanese aircraft.
At a time when the US Navy still considered it unsuitable for carrier use it was provided to the British Fleet Air Arm under Lend-Lease. The British Navy was desperately short of suitable high-performance fighters and therefore persevered with the Corsair, despite its problems, and the Fleet Air Arm's pilots quickly learned to cope with some of the aircraft's idiosyncracies. In any event improved versions, which amongst other things corrected the faults in the undercarriage, were later to became available.
The US Navy finally adopted the F4U as a shipboard fighter-bomber in November 1944, and by early 1945 large numbers were operating from the fast carriers of the Pacific Fleet - although the longer-established and very capable Grumman F6F Hellcat remained somewhat more numerous aboard the carriers right up to the war's end.
However, while the F6F was phased out shortly after World War Two the Corsair continued in service, and new versions were developed. The F4U was used extensively in the Korean War, and production continued until December 1952, by which time 12,571 had been built.
Specifications
Contractor:Chance Vought Division of United Aircraft Corporation (also built by Brewster and Goodyear)
Type: Single-seat Land and Carrier based fighter-bomber
Engines used:
(F4U-1) 2,000 hp Pratt & Whitney R-2800-8 (B) Double Wasp 18-cylinder two-row radial
(F4U-1A) 2,250 hp R-2800-8 (W) with water injection
(F4U-4) 2,450 hp R-2800-18 (W) with water-methanol
(F4U-5) 2,850 hp R-2800-32 (E) with water-methanol
Dimensions:
Span: 41' (12.48 metres) British version 39' 7"
Length: 33' 8" - 34' 6" according to version
Weight: (F4U-1A) 8,873 lb (4,025 kg)
Performance:
Maximum Speed: (F4U-1A) 395 mph (F4U-5) 462 mph
Initial Climb: (F4U-1A) 2,890 feet per minute (F4U-5) 4,800 feet per minute
Service Ceiling: F4U-1A) 37,000 feet (F4U-5) 44,000 feet
Range: (on internal fuel): 1,000 miles (1,609 kilometres)
Armaments:
Guns:
(early versions) 6 x 0.5" Browning MG53-2 machine-guns in outer wings, with 390 rounds per gun
(F4U-1C onwards) 4 x 20mm. cannon in wings
Bombs/Rockets:
(F4U-1D and most subsequent versions) 2 x 1,000 lb bombs or 8 x 5-inch rockets under wings
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