Thursday, June 18, 2009

Chance Vought F4U-ID CORSAIR

Military Papercraft
Chance Vought F4U-ID CORSAIR


View full image please click on image

F4U Corsair
An F4U-5NL, previously of the Honduran Air Force, at the Geneseo Airshow, with air intercept radar pod on right wing
Role Carrier-capable fighter aircraft
National origin United States
Manufacturer Chance Vought
First flight May 29, 1940
Introduction December 28, 1942
Primary users United States Navy
United States Marine Corps
Royal Navy
Royal New Zealand Air Force
Produced 1940-1952
Number built 12,571
Unit cost ?
Variants F2G "Super Corsair"


The Chance Vought F4U Corsair was a carrier-capable fighter aircraft that saw service in World War II and the Korean War (and in isolated local conflicts). Goodyear-built Corsairs were designated FG and Brewster-built aircraft F3A. The Corsair served in some air forces until the 1960s, following the longest production run of any piston-engined fighter in U.S. history (1942–1952).[1][2] Some Japanese pilots regarded it as the most formidable American fighter of World War II.[3] The U.S. Navy counted an 11:1 kill ratio with the F4U Corsair.[4]

Corsairs served with the U.S. Navy, U.S. Marines, Fleet Air Arm, and the Royal New Zealand Air Force, as well the French Navy Aeronavale and other services postwar. It quickly became the most capable carrier-based fighter-bomber of World War II. Demand for the aircraft soon overwhelmed Vought's manufacturing capability, resulting in production by Goodyear (as the FG-1) and Brewster (as the F3A-1). From the first prototype delivery to the U.S. Navy in 1940, to final delivery in 1953 to the French, 12,571 F4U Corsairs were manufactured by Vought,[5] in 16 separate models.[6][7]

Contents

[hide]

[edit] Development

In February 1938, the U.S. Navy Bureau of Aeronautics published two requests for proposal, for twin-engined and single-engined fighters. For the single-engined fighter the Navy requested the maximum obtainable speed, and a stalling speed not higher than 70 miles per hour (110 km/h). A range of 1,000 miles (1,600 km) was specified.[8] The fighter had to carry four guns, or three with increased ammunition. Provision had to be made for anti-aircraft bombs to be carried in the wing. These small bombs would, according to thinking in the 1930s, be dropped on enemy aircraft formations.

The XF4U-1 prototype in 1940/41

In June 1938, the U.S. Navy signed a contract for a prototype, the XF4U-1, BuNo 1443. The Corsair was designed by Rex Beisel and the Vought design team. After mock-up inspection in February 1939, construction of the XF4U-1 powered by an XR-2800-4 engine, rated at 1,805 hp (1,350 kW) went ahead quickly. When the prototype was built it had the biggest and most powerful engine, largest propeller and probably the largest wing on any fighter in history.[9] The first flight of the XF4U-1 was made on May 29, 1940, with Lyman A. Bullard, Jr. at the controls. The maiden flight proceeded normally until a hurried landing was made when the elevator trim tabs failed because of flutter.[10][11]

On October 1, the XF4U-1 made a flight from Stratford to Hartford with an average ground speed of 405 miles per hour (652 km/h), the first U.S. fighter to fly faster than 400 mph (640 km/h).[12] The XF4U-1 also had an excellent rate of climb. On the other hand, the testing of the XF4U-1 revealed some requirements would have to be rewritten. In full-power dive tests, speeds of up to 550 miles per hour (890 km/h) were achieved, not without damage to the control surfaces and access panels, and, in one case, an engine failure.[13] The spin recovery standards also had to be relaxed, as recovery from the required two-turn spin proved impossible without recourse to an anti-spin chute.[12] The problems clearly meant delays in getting the type into production.

Reports coming back from the war in Europe indicated that an armament of two .30 in (7.62 mm) (mounted in engine cowling) and two .50 in (12.7 mm) machine guns (one in each outer wing panel) was insufficient, and so when the U.S. Navy asked for production proposals in November 1940, heavier armament was specified.[14] The Navy entered into a letter of intent on March 3, 1941, received Vought's production proposal on April 2 and awarded Vought a contract for 584 F4U-1 fighters on June 30 of the same year.[15][16] It was a remarkable achievement for Vought; compared to land-based counterparts, carrier aircraft are "overbuilt" and heavier, to withstand the extreme stress of deck landings.

[edit] Design

2,000 hp (1,500 kW) Pratt & Whitney R-2800-8 in a Goodyear FG-1 Corsair

The F4U incorporated the largest engine available at the time, the 2,000 hp (1,490 kW) 18-cylinder Pratt & Whitney R-2800 Double Wasp radial. To extract as much power as possible, a relatively large, 13 feet 4 inches (4.1 m) Hamilton Standard Hydromatic three-blade propeller was used. To accommodate a folding wing, the designers considered retracting the main landing gear rearward, but for the chord of wing selected, it was difficult to fit undercarriage struts long enough to provide sufficient clearance for the large propeller. Their solution was an inverted gull wing, a similar layout to the one used by Germany's Junkers Ju 87 dive bomber, considerably shortening the length of the main gear legs.[17] The anhedral of the wing's center-section also permitted the wing and fuselage to meet at the optimum angle for minimizing drag, without the need for wing root fairings.[17] Offsetting these benefits, the bent wing was more difficult to construct and weighed more than a straight one.

The Corsair's aerodynamics were an advance over those of contemporary naval fighters. The F4U was the first U.S. Navy airplane to feature landing gear that retracted fully, in a similar manner to that of the Curtiss P-40 in that the oleo struts rotated through 90° during retraction, with the wheel atop the lower end of the strut; a pair of rectangular doors completely enclosed the wheel wells, leaving a completely streamlined wing.[18] The oil coolers were mounted in the center-section of the wings, alongside of the supercharger air intakes, and used openings in the leading edges of the wings, rather than protruding scoops. The large fuselage panels were made of magnesium and were attached to the frames with the newly-developed technique of spot welding, thus mostly eliminating the use of rivets. While employing this new technology, the Corsair was also the last American-produced fighter aircraft to feature fabric as the skinning for the top and bottom of each outer wing, aft of the main spar and armament bays, and for the ailerons, elevators and rudder. In addition, the elevators were constructed from plywood.[19] Even with its streamlining and high speed abilities, with full flap deployment of 60°, the Corsair could fly slowly enough for carrier landings.

In part because of its advances in technology and a top speed greater than existing Navy aircraft, numerous technical problems had to be solved before the Corsair would enter service. Carrier suitability was a major development issue, prompting changes to the main landing gear, tail wheel and tailhook. Early F4U-1s had difficulty recovering from developed spins, since the inverted gull wing's shape interfered with elevator authority. It also found that the Corsair's starboard wing could stall and drop rapidly and without warning during slow carrier landings. In addition, if the throttle were suddenly advanced (for example, during an aborted landing) the port wing could stall and drop so quickly that the fighter could flip over with the rapid increase in power.[20] These potentially lethal characteristics were later solved through the addition of a small, 6 in (152 mm)-long stall strip to the leading edge of the outer starboard wing, just inboard of the gun ports. This allowed the starboard wing to stall at the same time as the port.[21]

An early F4U-1 showing the "birdcage" canopy. Compare with the XF4U-1.

Other problems were encountered during early carrier trials. The combination of an aft cockpit and the Corsair's long nose made landings hazardous for newly-trained pilots. During landing approaches it was found that oil from the hydraulic cowl flaps could spatter onto the windscreen, badly reducing visibility, and the undercarriage oleo struts had bad rebound characteristics on landing, allowing the aircraft to bounce out of control down the carrier deck.[21] The first problem was solved by locking the top cowl flap down permanently, then replacing it with a fixed panel. The undercarriage bounce took more time to solve but eventually a "bleed valve" incorporated in the legs allowed the hydraulic pressure to be released gradually as the aircraft landed. The Corsair was not considered fit for carrier use until the wing stall problems and the deck bounce could be solved. In the event, because the more docile, and simpler to build F6F Hellcat had begun entering service, Corsair deployment aboard U.S. carriers was to be delayed until late 1944.[22][23]

Production F4U-1s featured several major modifications compared with the XF4U-1. A change of armament to six wing mounted .50 in (12.7 mm) M2 Browning machine guns (three in each outer wing panel) and their ammunition (400 rpg for the inner pair, 375 rpg for the outer)[24] meant that the location of the wing fuel tanks had to be changed. In order to keep the fuel tank close to the center of gravity (CG), the only available position was in the forward fuselage, ahead of the cockpit. Accordingly a 237 gal (897 l) self-sealing fuel tank replaced the fuselage mounted armament, the cockpit had to be moved back by 32 in (810 mm) and the fuselage lengthened.[17] In addition, 150lb of armor plate was installed, along with an 1.5 in (38 mm) bullet-proof windscreen which was set internally, behind the curved Plexiglas windscreen. The canopy could be jettisoned in an emergency and curved transparent panels, providing the pilot with a limited rear view over his shoulders, were inset into the fuselage, behind the pilot's headrest. A rectangular Plexiglas panel was inset into the lower center-section to allow the pilot to see directly beneath the aircraft and assist with deck landings.[25] The engine used was the more powerful R-2800-8 (B series) Double Wasp which produced 2,000 hp (1,491 kW). On the wings the flaps were changed to a NACA slotted type and the ailerons were increased in span to increase the roll rate, with a consequent reduction in flap span. IFF transponder equipment was fitted in the rear fuselage. All in all these changes increased the Corsair's weight by several hundred pounds.[26]

[edit] Operational history

[edit] United States Navy and Marine Corps

The performance of the Corsair was impressive. The F4U-1 was considerably faster than the F6F Hellcat and 13 mph (21 km/h) slower than the P-47 Thunderbolt,[27][28][29] the two other fighters 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 September 25, 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]

Early F4U-1s of VF-17.

Despite the decision to issue the F4U to Marine Corps units, two Navy units, VF-12 (October 1942) and later VF-17 (April 1943) were equipped with the F4U. By April 1943, VF-12 had successfully completed deck landing qualification.[36] However, VF-12 soon abandoned its aircraft to the Marines. VF-17 kept its Corsairs, but was removed from its carrier, USS Bunker Hill, due to perceived difficulties in supplying parts at sea.[37] In November 1943, while operating as a shore-based unit in the Solomon Islands, VF-17 reinstalled the tail hooks so its F4Us could land and refuel while providing top cover over the task force participating in the carrier raid on Rabaul. The squadron's pilots successfully landed, refueled and took off from their former home, Bunker Hill and the USS Essex on November 11, 1943.[38]

The U.S. Navy did not get into combat with the type until September 1943 and the Royal Navy's FAA would qualify the type for carrier operations first. The U.S. Navy finally accepted the F4U for shipboard operations in April 1944, after the longer oleo strut was fitted, which finally eliminated the tendency to bounce.[39] The first Corsair unit to be based effectively on a carrier was the pioneer USMC squadron, VMF-124, which joined Essex. They were accompanied by VMF-213. The increasing need for fighters as a protection against kamikaze attacks resulted in more Corsair units being moved to carriers.[40]

From February 1943 onward, the F4U operated from Guadalcanal and ultimately other bases in the Solomon Islands. A dozen USMC F4U-1s of VMF-124, commanded by Major William E. Gise, arrived at Henderson Field (code name "Cactus") on 12 February. The first recorded combat engagement was on February 14, 1943, when Corsairs of VMF-124 under Major Gise assisted P-40s and P-38s in escorting a formation of B-24 Liberators on a raid against a Japanese aerodrome at Kahili. Japanese fighters contested the raid and the Americans got the worst of it, with four P-38s, two P-40s, two Corsairs and two Liberators lost. No more than four Japanese Zeros were destroyed. A Corsair was responsible for one of the kills, although this was due to a midair collision. The fiasco was referred to as the "Saint Valentine's Day Massacre".[41][42] Although the Corsair's combat debut was not impressive, the Marines quickly learned how to make better use of the aircraft and started demonstrating its superiority over Japanese fighters. By May the Corsair units were getting the upper hand, and VMF-124 had produced the first Corsair ace, Second Lieutenant Kenneth A. Walsh, who would rack up a total of 21 kills during the war.[43]

I learned quickly that altitude was paramount. Whoever had altitude dictated the terms of the battle, and there was nothing a Zero pilot could do to change that we had him. The F4U could out-perform a Zero in every aspect except slow speed manoeuvrability and slow speed rate of climb. Therefore you avoided getting slow when combating a Zero. it took time but eventually we developed tactics and deployed them very effectively ... There were times, however, that I tangled with a Zero at slow speed one on one. In these instances I considered myself fortunate to survive a battle. Of my 21 victories, 17 were against Zeros and I lost five aircraft in combat. I was shot down three times and I crashed one that ploughed into the line back at base and wiped out another F4U.[44]

VMF-113 was activated on January 1, 1943 at Marine Corps Air Station El Toro as part of Marine Base Defense Air Group 41. They were shortly given their full complement of 24 F4U Corsairs. On March 26, 1944, while escorting 4 B-25 bombers on a raid over Ponape, they recorded their first enemy kills when they downed eight Japanese aircraft. In April of that year, VMF-113 was tasked with providing air support for the landings at Ujeland. Since the assault was unopposed the squadron quickly returned to striking Japanese targets in the Marshall Islands for the remainder of 1944.

Corsairs were flown by the famous "Black Sheep" Squadron (VMF-214, led by Marine Major Gregory "Pappy" Boyington) in an area of the Solomon Islands called "The Slot". Boyington was credited with 22 kills in F4Us (of 28 total, including six in an AVG P-40).[45] Other noted Corsair pilots of the period included VMF-124's Kenneth Walsh, James E. Swett, and Archie Donohue, VMF-215's Robert M. Hanson and Don Aldrich, and VF-17's Tommy Blackburn, Roger Hedrick, and Ira Kepford. Nightfighter versions equipped Navy and Marine units afloat and ashore.

At war's end, Corsairs were ashore on Okinawa, combating the kamikaze, and also were flying from fleet and escort carriers. VMF-312, VMF-323, VMF-224, and a handful of others met with success in the Battle of Okinawa.[46]

A Corsair fires its rockets at a Japanese stronghold on Okinawa

Corsairs also served well as fighter bombers in the Central Pacific and the Philippines. By spring 1944, Marine pilots were beginning to exploit the type's considerable capabilities in the close-support role during amphibious landings. Charles Lindbergh flew Corsairs with the Marines as a civilian technical advisor for United Aircraft Corporation in order to determine how best to increase the Corsair's payload and range in the attack role and to help evaluate future viability of single- versus twin-engine fighter design for Vought.[47] Lindbergh managed to get the F4U into the air with 4,000 pounds (1,800 kg) of bombs, with a 2,000 pounds (910 kg) bomb on the centerline and a 1,000 pounds (450 kg) bomb under each wing.[48] In the course of such experiments, he performed strikes on Japanese positions during the battle for the Marshall Islands.[47]

By the beginning of 1945, the Corsair was a full-blown "mudfighter", performing strikes with high-explosive bombs, napalm tanks, and HVARs. She proved surprisingly versatile, able to operate everything from Bat glide bombs (without sacrificing a load of 2.75 in/70 mm rockets) to 11.75 in (300 mm) Tiny Tim rockets.[49] The aircraft was a prominent participant in the fighting for the Palaus, Iwo Jima and Okinawa.

Statistics compiled at the end of the war indicate that the F4U and FG flew 64,051 operational sorties for the U.S. Marines and U.S. Navy through the conflict (44% of total fighter sorties), with only 9,581 sorties (15%) flown from carrier decks.[50] F4U and FG pilots claimed 2,140 air combat victories against 189 losses to enemy aircraft, for an overall kill ratio of over 11:1.[51] The aircraft performed well against the best Japanese opponents with a 12:1 kill ratio against Mitsubishi A6M and 6:1 against the Nakajima Ki-84, Kawanishi N1K-J and Mitsubishi J2M combined during the last year of the war.[52] The Corsair bore the brunt of fighter-bomber missions, delivering 15,621 tons (14,171 tonnes) of bombs during the war (70% of total bombs dropped by fighters during the war).[51]

Corsair losses in World War II were as follows:

  • By combat: 189
  • By enemy anti-aircraft artillery: 349
  • Accidents during combat missions: 230
  • Accidents during non-combat flights: 692
  • Destroyed aboard ships or on the ground: 164[51]

One particularly interesting kill was scored by a Marine Lieutenant R. R. Klingman of VMF-312 Checkerboards, over Okinawa. Klingman was in pursuit of a Kawasaki Ki-45 Toryu ("Nick") twin engine fighter at extremely high altitude when his guns jammed due to the gun lubrication thickening from the extreme cold. He simply flew up and chopped off the Ki-45's tail with the big propeller of the Corsair. Despite missing five inches (127 mm) off the end of his propeller blades, he managed to land safely after this ramming attack. He was awarded the Navy Cross.[53]

[edit] Korean War

During the Korean War, the Corsair was used mostly in the close-support role. The AU-1 Corsair was a ground-attack version produced for the Korean War; its Pratt & Whitney R-2800 engine, while supercharged, was not as highly boosted as on the F4U. As the Corsair moved from its air superiority role in World War II into the close air support role in the Korean Conflict, the gull wing proved to be a useful feature. A straight, low-wing design would have blocked most of the visibility from the cockpit toward the ground while in level flight, but a Corsair pilot could look through a "notch" and get a better ground reference without having to bank one way or the other to move the wing out of the way.[citation needed]

The AU-1, F4U-4B, -4C, -4P and -5N logged combat in Korea between 1950 and 1953.[54] There were dogfights between F4Us and Soviet-built Yakovlev Yak-9 fighters early in the conflict, but when the enemy introduced the Mikoyan-Gurevich MiG-15, the Corsair was outmatched, though one Marine pilot did get lucky. On September 10, 1952, a MiG-15 made the mistake of getting into a turning contest with a Corsair piloted by Captain Jesse G. Folmar, with Folmar shooting the MiG down with his four 20 millimetres (0.79 in) cannon.[55] The MiG's wingmen quickly had their revenge, shooting down Folmar, though he bailed out and was swiftly rescued with little injury.

Corsair night fighters were used to an extent. The enemy adopted the tactic of using low-and-slow Polikarpov Po-2 intruders to perform night harassment strikes on American forces, and jet-powered night fighters found catching these "Bedcheck Charlies" troublesome. U.S. Navy F4U-5Ns were posted to shore bases to hunt them down, with U.S. Navy Lieutenant Guy Pierre Bordelon, Jr. becoming the Navys only ace in the conflict, as well as the only ace to not score any victories in a jet aircraft.[56] "Lucky Pierre" was credited with five kills (two Yakovlev Yak-18 and three Po-2).[55] Navy and Marine Corsairs were credited with a total of 12 enemy aircraft.[55]

More generally, Corsairs performed attacks with cannon, napalm tanks, various iron bombs and unguided rockets. The old HVAR was a reliable standby; however sturdy Soviet-built armor proved resistant to the HVAR's punch. This led to a new 6.5 in (16.5 cm) shaped charge antitank warhead being developed. The result was called the "Anti-Tank Aircraft Rocket (ATAR)." Tiny Tim was also used in combat, with two under the belly.[57] There is also a story of a Corsair pilot who used his arresting hook to snag enemy communications lines from telephone poles.[58]

Lieutenant Thomas J. Hudner, Jr., flying with naval squadron VF-32 off the USS Leyte, was awarded the Medal of Honor for crash landing his Corsair in an attempt to rescue his squadron mate, Ensign Jesse L. Brown, whose aircraft had been forced down by antiaircraft fire near Changjin. Brown, who did not survive the incident, was the U.S. Navy's first African American naval aviator.[59][60]

[edit] Royal Navy

FG-1D Corsair in FAA markings

In the early days of the war, Royal Navy fighter requirements had been based on cumbersome two-seat designs, such as the Blackburn Skua (and its turreted derivative the Blackburn Roc) as well as the Fairey Fulmar, on the assumption they would only be fighting long range bombers or flying boats. The Royal Navy hurriedly adopted higher performance aircraft such as the Hawker Sea-Hurricane and the less robust Supermarine Seafire but neither of these aircraft had sufficient range to operate at a distance from a carrier task force. The Corsair was welcomed as a much more robust and versatile alternative.[61]

In Royal Navy service, because of the limited hanger deck height in several classes of British carrier, many Corsairs had their outer wings "clipped" by 8 in (200 mm) to clear the deckhead.[62] The change in span brought about the added benefit of improving the sink rate, reducing the F4U's propensity of "floating" in the final stages of landing.[62] Despite the clipped wings and the shorter decks of British carriers, Royal Navy aviators found landing accidents less of a problem than they had been to U.S. Navy aviators due to the curved approach used. British units solved the landing visibility problem by approaching the carrier in a medium left-hand turn, which allowed the pilot to keep the carrier's deck in view over the dip in the port wing, allowing safe carrier operations.[63]

The Royal Navy developed a number of modifications to the Corsair that made carrier landings more practical. Among these are the Malcolm Hood, raising the pilot's seat 7 in (180 mm)[64] and wiring "shut the cowl flaps across the top of the engine compartment, diverting the oil and hydraulic fluid around the sides of the fuselage".[65]

The Royal Navy received 95 Corsair Mk Is and 510 Mk IIs, these being equivalent to the F4U-1 and -1A. Brewster-built aircraft were known as Mk IIIs (equivalent to F3A-1D), and Goodyear-built aircraft were known as Mk IVs (equivalent to FG-1D). The Mk IIs and Mk IVs were the only versions to be used in combat.[66] The Royal Navy cleared the F4U for carrier operations well before the U.S. Navy and showed that the Corsair Mk II could be operated with reasonable success even from escort carriers. It was not without problems, one being excessive wear of the arrester wires due to the weight of the Corsair and the understandable tendency of the pilots to stay well above the stalling speed. A total of 2,012 Corsairs were supplied to the United Kingdom.[33]

Fleet Air Arm units were created and equipped in the United States, at Quonset Point or Brunswick and then shipped to war theaters aboard escort carriers. The first FAA Corsair unit was No. 1830, created on the first of June 1943, and soon operating from HMS Illustrious. At the end of the war, 18 FAA squadrons were operating the Corsair. British Corsairs served both in Europe and in the Pacific. The first, and also most important, European operations were the series of attacks (Operation Tungsten) in April, July and August 1944 on the German battleship Tirpitz, for which Corsairs from HMS Victorious and HMS Formidable provided fighter cover.[67] It appears the Corsairs did not encounter aerial opposition on these raids.

At least one Corsair was captured by the Germans, this was Corsair JT404 from No. 1841 squadron (Formidable). Wing Leader Lieutenant Commander RS Baker-Falkner made an emergency landing on July 18, 1944] in a field at Sorvag, near Bodø, Norway. The Corsair was captured intact, although it is not known if it was taken to Germany.[68]

In the Pacific, FAA Corsairs began to operate with the British Pacific Fleet in April 1944, participating in an attack on Sabang, and later, on January 24 and January 30, 1945 (code-named Meridian One and Meridian Two respectively) attacked the oil refineries at Palembang. In July and August 1945, Corsair squadrons Nos. 1834, 1836, 1841 and 1842 took part in a series of strikes on the Japanese mainland, near Tokyo. These squadrons operated from Victorious and Formidable.[69]

On August 9, 1945, days before the end of the war, FAA Corsairs from Formidable were attacking Shiogama harbor on the northeast coast of Japan. Royal Canadian Navy pilot, Lieutenant Robert Hampton Gray, of 1841 Squadron was hit by flak but pressed home his attack on a Japanese destroyer, sinking it with a 1,000 pounds (450 kg) bomb but crashing into the sea. He was posthumously awarded Canada's last Victoria Cross, becoming the second fighter pilot of the war to earn a Victoria Cross as well as the final Canadian casualty of World War II.[70]

FAA Corsairs originally fought in a camouflage scheme with a Dark Slate Grey/Extra Dark Sea Grey disruptive pattern on top and Sky undersides, but were later painted overall dark blue. Those operating in the Pacific theater acquired a specialized British insignia — a modified blue-white roundel with white "bars" to make it look more like a U.S. than a Japanese Hinomaru insignia to prevent friendly-fire incidents.

In all, out of eighteen carrier-based squadrons eight saw combat, flying intensive ground attack/interdiction operations and claiming 47.5 aircraft shot down.[71]

[edit] Royal New Zealand Air Force

Equipped with obsolescent Curtiss P-40s, Royal New Zealand Air Force (RNZAF) squadrons in the South Pacific performed impressively compared to the American units they operated alongside, in particular in the air-to-air role. The American government accordingly decided to give New Zealand early access to the Corsair, especially as it was not initially being used from carriers. Some 424 Corsairs equipped 13 RNZAF squadrons, including No. 14 Squadron RNZAF and No. 15 Squadron RNZAF, replacing SBD Dauntless as well as P-40s.[72] The F4Us were allocated NZ prefixed serial numbers: F4U-1s[73] NZ5201 to NZ5299; NZ5300 to NZ5399; NZ5400 to NZ5487, all of which were assembled by Unit 60; NZ5500 to NZ5577 were assembled and flown at RNZAF Hobsonville. In total there were 237 F4U-1s and 127 F4U-1Ds used by the RNZAF during the Second World War. 60 FG-1Ds which arrived post war were given serial numbers prefixed NZ5600 to NZ5660.[74]

The first deliveries of lend-lease Corsairs began in March 1944 with the arrival of 30 F4U-1s at the RNZAF Base Depot Workshops (Unit 60) at Espiritu Santo in the New Hebrides. From April, these workshops became responsible for assembling all Corsairs for the RNZAF units operating the aircraft in the South West Pacific and a Test and Despatch flight was set up to test the aircraft after assembly. By June 1944, 100 Corsairs had been assembled and test flown.[72] The first squadrons to use the Corsair were 20 and 21 Squadrons on Espiritu Santo island, operational in May 1944. The organization of the RNZAF in the Pacific and New Zealand meant that only the pilots and a small staff belonged to the Squadron (the maximum strength on a squadron was 27 pilots): Squadrons were assigned to several Servicing Units (SUs 5-6 officers, 57 NCOs, 212 airmen) which carried out aircraft maintenance and operated from fixed locations:[75] hence F4U-1 NZ5313 was first used by 20 Squadron/1 SU on Guadalcanal in May 1944; 20 Squadron was then relocated to 2 SU on Bougainville in November.[76] In all there were 10 frontline SUs plus another three based in New Zealand. Because each of the SUs painted its aircraft with distinctive markings[77] and the aircraft themselves could be repainted in several different colour schemes the RNZAF Corsairs were far less uniform in appearance compared with their American and FAA contemporaries.[78] By late 1944, the F4U had equipped all ten Pacific-based fighter squadrons of the RNZAF.[74]

By the time the Corsairs arrived, there were virtually no Japanese aircraft left in New Zealand's allocated sectors of the Southern Pacific, and despite the RNZAF Squadrons extending their operations to more northern islands, they were primarily used for close support of American, Australian and New Zealand soldiers fighting the Japanese. New Zealand pilots were aware of the Corsair's poor forward view and tendency to ground loop, but found these drawbacks could be solved by pilot training in curved approaches before use from rough forward airbases.[citation needed] At the end of 1945, all Corsair squadrons but one (No. 14) were disbanded. That last squadron was based in Japan, until the Corsair was retired from service in 1947.[79]

No. 14 Squadron was given new FG-1Ds and, in March 1946 transferred to Iwakuni, Japan as part of the British Commonwealth Occupation Force. Only one airworthy example of the 424 aircraft procured survives: NZ5648/ZK-COR, owned by the Old Stick and Rudder Company at Masterton, NZ. One other mostly complete aircraft and the remains of two others were known to be held by a private collector at Ardmore, NZ, in 1996. Their current whereabouts are unknown.[80][81]

[edit] French Navy

A total of 94 F4U-7s were built for the French Navy in 1952, with the last of the batch, the final Corsair built, rolled out on December 24, 1952.[82] The F4U-7s were actually purchased by the U.S. Navy and passed on to the Aeronavale through the U.S. Military Assistance Program (MAP). The French used their F4U-7s during the end of the First Indochina War in the 1950s, where they were supplemented by at least 25 ex-USMC AU-1s passed on to the French in 1954, after the end of the Korean War.[83]

French Corsairs also performed strikes in the Algerian War in 1955 and 1956 and assisted in the Anglo-French-Israeli seizure of the Suez Canal in October 1956, codenamed Operation Musketeer. The Corsairs were painted with yellow and black recognition stripes for this operation. In 1960, some French Corsairs were rigged to carry four SS-11 wire-guided missiles. This was a more or less experimental fit and it is hard to believe it worked well, since it required a pilot to "fly" the missile after launch with a joystick while keeping track of a flare on its tail — an exercise that could be very tricky in a single-seat aircraft under combat conditions. All French Corsairs were out of service by 1964, with some surviving for museum display or as civilian warbirds.[80]

[edit] "Football War"

Corsairs flew their final combat missions during the 1969 "Football War" between Honduras and El Salvador, in service with both air forces. The conflict was famously triggered, though not really caused, by a disagreement over a football (soccer) match. Both sides claimed various numbers of kills, and each side disputed the claims of the other.[84] At the outset of the Football War, El Salvador enlisted the assistance of several American pilots with P-51 and F4U experience. Bob Love, a Korean was ace, Chuck Lyford, Ben Hall and Lynn Garrison flew in the world's last combat between propeller-driven fighters. Lynn Garrison had purchased F4U-7 133693 from the French MAAG office when retired from French naval service in 1964.[citation needed]

[edit] Legacy

The Corsair entered service in 1942. Although designed as a carrier fighter, initial operation from carrier decks proved to be troublesome. Its low-speed handling was tricky due to the port wing stalling before the starboard wing. This factor, together with poor visibility over the long nose (leading to one of its nicknames, "The Hose Nose"), made landing a Corsair on a carrier a difficult task. For these reasons, most Corsairs initially went to Marine Corps squadrons who operated off land-based runways, with some early Goodyear built examples (designated FG-1A) being built with fixed, non-folding wings.[33] The USMC aviators welcomed the Corsair with open arms as its performance was far superior to the contemporary Brewster Buffalo and Grumman F4F-3 and -4 Wildcat.

Moreover, the Corsair was able to outperform the primary Japanese fighter, the A6M Zero. While the Zero could out-turn the F4U at low speed, the Corsair was faster and could out-climb and out-dive the A6M.[85] Tactics developed early in the war, such as the Thach Weave, took advantage of the Corsair's strengths.

This performance advantage, combined with the ability to take severe punishment, meant a pilot could place an enemy aircraft in the killing zone of the F4U's six .50 (12.7 mm) M2 Browning machine guns and keep him there long enough to inflict major damage. The 2,300 rounds carried by the Corsair gave over one full minute of fire from each gun, which, fired in three to six-second bursts, made the F4U a devastating weapon against aircraft, ground targets, and even ships.

Beginning in 1943, the Fleet Air Arm (FAA) also received Corsairs and flew them successfully from Royal Navy carriers in combat with the British Pacific Fleet and in Norway.[86] These were clipped-wing Corsairs, the wingtips shortened 8 in (20 cm) to clear the lower overhead height of RN carriers. FAA also developed a curving landing approach to overcome the F4U's deficiencies.[87]

Infantrymen nicknamed the Corsair "The Sweetheart of the Marianas" and "The Angel of Okinawa" for its roles in these campaigns. Among Navy and Marine aviators, however, the aircraft was nicknamed "Ensign Eliminator" and "Bent-Wing Eliminator" because it required many more hours of flight training to master than other Navy carrier-borne aircraft. It was also called simply "U-bird" or "Bent Wing Bird".[5] The Japanese allegedly nicknamed it "Whistling Death", for the noise made by airflow through the wing root-mounted oil cooler air intakes.[7][88]

The Corsair has been named the official aircraft of Connecticut,[89] due to its connection with Sikorsky Aircraft, in legislation sponsored by state senator George "Doc" Gunther; Gunther had also organized a Corsair Celebration and Symposium at Sikorsky Memorial Airport in Stratford, Connecticut, on Memorial Day, May 29, 2006.[90]

[edit] Variants

Underside of a Corsair
Royal Navy Corsair Mk.Is

During World War II, Corsair production expanded beyond Vought to include Brewster and Goodyear models. Allied forces flying the aircraft in World War II included FAA and RNZAF. Eventually, more than 12,500 F4Us would be built, comprising 16 separate variants.[6]

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.[91] 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 (9.7 m) to 33 feet 4 inches (10.2 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]

F4U-1A (Corsair Mk II): The designation F4U-1A does not appear in lists of Corsair Bureau Numbers and was not in official use, being applied post-war to differentiate mid to late production F4U-1s from the early production variant.[26][94] Mid to late production Corsairs incorporated a new, taller and wider clear-view canopy with only two frames, along with a simplified clear view windscreen. The cockpit seat was raised 7 in (178 mm) which, with the wider canopy top section, allowed the pilot better visibility over the long nose. The Plexiglas rear-view windows as well as the one under the cockpit were omitted. The tailwheel strut was lengthened, which also aided the pilot's forward view. These Corsairs were the first "carrier capable" variant and introduced a 6 in (152 mm)-long stall strip just outboard of the gun ports on the starboard wing leading edge and improved undercarriage oleo struts which eliminated bouncing on landing. F4U-1s supplied to the USMC lacked arrester hooks and the tail wheels were changed to a smaller diameter solid rubber type.[95] Additionally, an experimental R-2800-8W engine with water injection was fitted on one of the late F4U-1As. After satisfactory results, many F4U-1As were fitted with the new powerplant. The aircraft carried 237 gal (897 l) in the main fuel tank, located in front of the cockpit, as well as an unarmored, non-self-sealing 62 gal (235 l) fuel tank in each wing. This version of the Corsair was the first to be able to carry a drop tank under the center-section. With drop tanks fitted, the fighter had a maximum ferry range of just over 1,500 mi (2,400 km).

A land-based version, without the folding wing capability, was built by Goodyear as the FG-1A. In British service, the aircraft type was modified with "clipped" wings (8 inches (200 mm) was cut off each wingtip) for use on British aircraft carriers,[92] under the designation Corsair Mk II.

F3A-1 (Corsair Mk. III):This was the designation for the Brewster built F4U-1. Just over 700 were built before Brewster was forced out of business. Poor production techniques and shabby quality control meant that these aircraft were red-lined for speed and prohibited from aerobatics after several lost their wings. This was later traced to poor quality wing fittings. None of the Brewster built Corsairs reached front-line units.[96]

F4U-1B: This was an unofficial post-war designation used to identify F4U-1s modified for FAA use.[26]

F4U-1C:The prototype F4U-1C, BuNo50277, appeared in August 1943 and was based on an F4U-1. 200 of this variant were built from July through to November 1944: all were based on the F4U-1D and were built in parallel with that variant.[72] Intended for ground-attack as well as fighter missions, the F4U-1C was similar to the F4U-1D but its armament was replaced by four 20 millimetres (0.79 in) AN/M2 cannons with 231 rpg[97] of ammunition. The F4U-1C was introduced to combat during 1945, most notably in the Okinawa campaign. Aviators preferred the standard armament of six .50 in (12.7 mm) machine guns since they were already more than powerful enough to destroy most Japanese aircraft, and had more ammunition and a higher rate of fire.[98] The weight of the Hispano cannons and their ammunition affected the flight performance, especially its agility, but the aircraft was found to be especially potent in the ground attack role.

An FG-1D with the later style canopy used by the F4U-1D.

F4U-1D (Corsair Mk IV): Built in parallel with the F4U-1C, but was introduced in April 1944. It had the new -8W water-injection engine. This change gave the aircraft up to 250 hp (187 kW) more power, which, in turn, increased performance. Speed, for example, was boosted from 417 miles per hour (671 km/h) to 425 miles per hour (684 km/h). Because of the U.S. Navy's need for fighter-bombers, it had a payload of rockets double the -1A's, as well as twin-rack plumbing for an additional belly drop tank. Such modifications necessitated the need for rocket tabs (attached to fully metal-plated underwing surfaces) and bomb pylons to be bolted on the fighter, however, causing extra drag. Additionally, the new job of fighter-bombing was a new task for the Corsair and the wing fuel cells proved too vulnerable and were removed.[citation needed] The extra fuel carried by the two drop tanks would still allow the aircraft to fly relatively long missions despite the heavy, un-aerodynamic load. The regular armament of six machine guns were implemented as well. The canopies of most -1Ds had their struts removed along with their metal caps, which were used — at one point — as a measure to prevent the canopies' glass from cracking as they moved along the fuselage spines of the fighters.[citation needed] Also, the clear-view style "Malcolm Hood" canopy used initially on Supermarine Spitfire and P-51C Mustang aircraft was adopted as standard equipment for the -1D model, and all later F4U production aircraft. Additional production was carried out by Goodyear (FG-1D) and Brewster (F3A-1D). In Fleet Air Arm service, the latter was known as the Corsair III, and both had their wingtips clipped by 8" per wing to allow storage in the lower hangars of British carriers.[92]

F4U-1P: A rare photo reconnaissance variant.[99]

An F4U-2. The radome on the starboard outer wing is just visible.

XF4U-2: Special night fighter variant, equipped with two auxiliary fuel tanks.[100]

F4U-2: Experimental conversion of the F4U-1 Corsair into a carrier-borne night fighter, armed with five .50 in (12.7 mm) machine guns (the outboard, starboard gun was deleted), and fitted with airborne Intercept (AI) radar set in a radome placed outboard on the starboard wing. Since Vought was preoccupied with more important projects, only 32 were converted from existing F4U-1s by the Naval Aircraft Factory and another two by front line units.[101][102]

The type saw combat with VF(N)-101 aboard USS Enterprise and USS Intrepid in early 1944, VF(N)-75 in the Solomons and VMF(N)-532 on Tarawa.

XF4U-3: Experimental aircraft built to hold different engines in order to test the Corsair's performance with a variety of power plants. This variant never entered service. Goodyear also contributed a number of airframes, designated FG-3, to the project. A single sub-variant XF4U-3B with minor modifications was also produced.[103] XF4U-3B, planned procurement for the FAA.[100]

XF4U-4: New engine and cowling.[100]

F4U-4: The last variant to be produced during World War II, the F4U-4 began entering service near the end of 1944. It fully equipped naval squadrons four months before the end of hostilities. It had the 2,100 hp (1,566 kW) dual-stage-supercharged -18W engine. When the cylinders were injected with the water/alcohol mixture, power was boosted to 2,450 hp (1,827 kW). The aircraft required an air scoop under the nose and the unarmored wing fuel tanks of 62 gal (234 l) capacities were removed for better maneuverability at the expense of maximum range. The propeller had one additional blade, bringing the total to four. Maximum speed was increased to 448 miles per hour (721 km/h) and climb rate to over 3,800 ft/min (1,180 m/min) as opposed to the 2,900 ft/min (884 m/min) of the F4U-1A. The service ceiling also increased significantly from 37,000 feet (11,000 m) to 41,000 feet (12,000 m).[citation needed] The "4-Hog" retained the original armament and had all the external loads (i.e., drop tanks, bombs) capabilities of the F4U-1D. The windscreen was now flat bullet-resistant glass to avoid optical warping, a change from the curved Plexiglas windscreens with the internal plate glass of the earlier Corsairs.[citation needed] Vought also tested the two F4U-4Xs (BuNos 49763 and 50301, prototypes for the new R2800) with fixed tiptanks (the Navy showed no interest) and an Aeroproducts six-blade contraprop (not accepted for production).[104]

An F4U-4 of VF-1b on board USS Midway, 1947-1948.

F4U-4B: Designation for F4U-4s to be delivered to the British Fleet Air Arm, but were retained by the U.S. for its own use. The Fleet Air Arm received no F4U-4s.[105]

F4U-4C: 300 F4U-4s ordered with alternate gun armament of four 20 millimetres (0.79 in) AN/M2 cannons.[105]

F4U-4E and F4U-4N: Developed late in the conflict, these night fighters featured radar radomes projecting from the starboard wingtip. The -4E was fitted with the APS-4 search radar, while the -4N was fitted with the APS-6 type. In addition, these aircraft were often refitted with four 20mm M2 cannons similar to the F4U-1C. The night fighter variants would see greater use during the Korean conflict.[106]

F4U-4K: Experimental drone.[100]

F4U-4P: As with the -1P, a rare photo reconnaissance variant.[99]

XF4U-5: New engine cowling, other extensive changes.[100]

F4U-5: A 1945 design modification of the F4U-4, first flown on December 21st of that year, was intended to increase the F4U-4 Corsair's overall performance and incorporate many Corsair pilots' suggestions. It featured a more powerful Pratt and Whitney R-2800-32(E) engine with a two stage supercharger,[107] rated at a maximum of 2,450 hp (1,830 kW). Other improvements included automatic blower controls, cowl flaps, intercooler doors and oil cooler for the engine, spring tabs for the elevators and rudder, a completely modernized cockpit, a completely retractable tail wheel, and heated cannon bays and pitot head. The cowling was lowered two degrees to help with forward visibility, but perhaps most striking as the first variant to feature all-metal wings (223 units produced).[108]

F4U-5N: Radar equipped version (214 units produced)

F4U-5NL: Winterized version (72 units produced,[109] 29 modified from F4U-5Ns (101 total). Fitted with rubber de-icing boots on the leading edge of the wings and tail.[110]

F4U-5P: Long-range photo-reconnaissance version (30 units produced)

F4U-6: Redesignated AU-1, this was a ground-attack version produced for the U.S. Marine Corps.

F4U-7 : AU-1 developed for the French Navy.

FG-1E: Goodyear FG-1 with radar equipment.[100]

FG-1K: Goodyear FG-1 as drone.[100]

FG-3: Turbosupercharger version converted from FG-1D.

FG-4:Goodyear F4U-4, never delivered.[100]

[edit] Super Corsair variants

The F2G-1 and F2G-2 were significantly different aircraft, fitted with the Pratt & Whitney R-4360 Wasp Major 4-row 28-cylinder "corncob" radial engine and teardrop (bubble) canopy, as a specialized interceptor against kamikaze attacks. The difference between the -1 and -2 variants was that the -1 featured a manual folding wing and 14 ft (4.3 m) Propellers, while the F2G-2 aircraft had hydraulic operated folding wings, 13 ft (4.0 m) propellers and carrier arresting hooks for carrier use.[111] As World War II was drawing to a close, development problems emerged that led to the abandonment of further work on the F2G series.[112] While only 10 were built, several F2Gs went on to racing success after the war, winning the Thompson trophy races in 1947 and 1949.

[edit] Operators

An French Navy F4U-7 Corsair of 14.F flotilla
Corsair FG-1D (Goodyear built F4U-1D) in the Royal New Zealand Air Force markings
Argentina
El Salvador
France
Honduras
New Zealand
United Kingdom
United States

[edit] Survivors

F4U-4 #97369 on display at the National Museum of the Marine Corps
Vought F4U-4 #97388 at Corsairs Over Connecticut event, June 2005
F2G-1 "Super Corsair" #88458, painted as Race #57, owned by Bob Odergaard of Kindred, North Dakota, flying at the 2005 AirVenture at Oshkosh, Wisconsin.
Goodyear FG-1D at Wings Over the Rockies Museum, Denver, CO, modified as racer N194G.
F/A-18F Super Hornet flying alongside an F4U at the Miramar Air Show in 2008

Chance-Vought F4U survivors Over two dozen Corsairs are believed to be still airworthy, most in the United States. Others are found in museum collections worldwide.

  • FG-1D 92436: In flying condition (currently undergoing complete restoration in Idaho) Owner: Olympic Flight Museum, Olympia airport, Olympia, Washington
  • FG-1D 92106: 17,000 hour restoration completed in 2003 by Airpower Unlimited, judged as 2003 Oshkosh E.A.A. Airventure Grand Champion Warbird - World War II and 2003 - Rolls Royce - Heritage Trophy Reno, Nevada - People's Choice Trophy. Acquired in 2007 by Vintage Wings of Canada, Ottawa/Gatineau Airport(CYND), Canada and flown regularly for commemorative events.[113]
  • FG-1D #88382: on static display in the Personal Courage Wing of The Museum of Flight, Seattle, Washington
  • F4U-1A #17799: in flying condition at the Planes of Fame Air Museum, Chino, California
  • F4U-1D #50375: on static display at the Smithsonian Air and Space Museum's Steven F. Udvar-Hazy Center, Chantilly, Virginia. This aircraft was autographed in the wheel well in Magic Marker by "Pappy" Boyington when it was previously on display at the NASM's Garber Restoration and Storage Facility in Silver Hill, Maryland. The autograph is still visible, though the aircraft hangs from the ceiling.
  • XF4U-4 #80750: on static display at the New England Air Museum, Windsor Locks, Connecticut
  • F4U-4 #97142: on static display at the Pima Air & Space Museum, Tucson, Arizona
  • F4U-4 #97280 / NX712RD: on static display at the Cavanaugh Flight Museum, Addison, Texas
  • F4U-4 #97286: Angel of Okinawa on static display at the Fantasy of Flight Museum, Polk City, Florida. This aircraft was owned by Merle B. Gustafson from 1972 until 1984.
  • F4U-4 #97349: on static display at the National Museum of Naval Aviation, NAS Pensacola, Florida
  • F4U-4 #97369: on static display at the National Museum of the Marine Corps, Quantico, Virginia
  • F4U-4: in flying condition, owned by The Flying Bulls, Salzburg, Austria. Registration: OE-EAS
  • F4U-5N #121881: former Argentine Navy aircraft (c/n 121881, COAN serial 0389), although missing its radome, restored in the colors of Lt. Guy Bordelon. Flying as a night fighter in Korea as a member of VC-3 Squadron, U.S. Navy, Lt. Bordelon was the only U.S. ace in Korea who flew a propeller driven airplane. Lone Star Flight Museum, Galveston, Texas
  • F4U-5N #122189: on static display at the Flying Leatherneck Aviation Museum, MCAS Miramar, California[114]
  • F4U-5N: In flying condition, served with the Honduran Air Force and saw combat in the ground-attack role in 1969 against El Salvador. Formerly at the Indiana Aviation Museum, Valparaiso, Indiana; sold to a private party in 2008.
  • F4U-7 #133704: on static display at the USS Alabama Battleship Memorial Park, Mobile, Alabama
  • F2G-1 "Super Corsair" NX4324: Restored by Doug Champlin is on display in the Great Gallery of the Museum of Flight in Seattle Washington.
  • F2G-1 "Super Corsair" #88458: in flying condition, painted as Race #57 at the Fargo Air Museum, Fargo, North Dakota
  • F2G-1D "Super Corsair" #88463: Race No. 74 was sold to Walter Soplata, of Newberry, Ohio. This F2G was acquired by the Crawford Auto-Aviation Museum in Cleveland, Ohio. Bob Odergaard of Kindred, North Dakota is restoring the aircraft to static condition.
  • F4U-5 #121928: last remaining in Argentina (c/n 121928, COAN serial 0391), on static display as 3-A-211 at the Museo de la Aviacion Naval, Espora Naval Air Base, Bahía Blanca, Argentina.
  • F4U-7 #133704 (not original Bu#): in flying condition, restored as a Flotille (Squadron ) 14F, Marine Nationale (French Navy). Originally a former F4U-5NL Argentine Navy aircraft (Bu#124541, COAN serial 0433, 3-A-204) which was on static display at the Museo Naval de la Nacion, Tigre, Argentina. Sold in 1991, currently privately owned in France.
  • F4U-1 at TAM Wings of a Dream Museum, São Carlos, Brazil. Donated by Pratt & Whitney. This airplane was part of USMC VMF-122. The museum claims it is the oldest Corsair still in flying conditions (left factory on October 19, 1943).

[edit] Specifications

[edit] F4U-1A

Data from Aeroweb[115]

General characteristics

  • Crew: 1 pilot
  • Length: 33 ft 4 in (10.1 m)
  • Wingspan: 41 ft 0 in (12.5 m)
  • Height: 16 ft 1 in (4.90 m)
  • Wing area: 314 ft2 (29.17 m2)
  • Empty weight: 8,982 lb (4,073 kg)
  • Loaded weight: 14,000 lb (6,300 kg)
  • Powerplant:Pratt & Whitney R-2800-8W radial engine, 2,250 hp (1,678 kW)

Performance

Armament

[edit] F4U-4

Data from Aeroweb[116]

General characteristics

  • Crew: 1 pilot
  • Length: 33 ft 8 in (10.2 m)
  • Wingspan: 41 ft 0 in (12.5 m)
  • Height: 14 ft 9 in (4.50 m)
  • Empty weight: 9,205 lb (4,174 kg)
  • Loaded weight: 14,669 lb (6,653 kg)
  • Powerplant:Pratt & Whitney R-2800-18W radial engine, 2,450 hp (1,827 kW)

Performance

Armament

  • Guns:
  • Rockets: 8 × 5 in (12.7 cm) high velocity aircraft rockets and/or
  • Bombs: 4,000 pounds (1,800 kg)

[edit] Popular culture

  • Flying Leathernecks (1951) starring John Wayne, was about a Marine Corps squadron flying Corsairs while developing close-support tactics.
  • The exploits of Marine Corps squadron VMF-214, which flew the Corsair in the Pacific during the war, were depicted in the popular 1976 made-for-television movie Baa Baa Black Sheep (also released as Flying Misfits) and the follow-up television series Baa Baa Black Sheep, which aired from 1976 to 1978). The television series featured six genuine flying Corsairs, but the storylines were fictional. See also Pappy Boyington.
  • The Corsair plays a prominent role in W.E.B. Griffin's book series, The Corps (1986–present).
  • Ted Williams served as a flight instructor training young Marines to fly Corsairs while away from major league baseball during his years of military service in World War II.


Download Papercraft Model : Click Here

MIRAGE 2000

Military Papercraft
MIRAGE 2000


View full image please click on image

Mirage 2000
A Mirage 2000-5F of the French Air Force
Role Multirole fighter aircraft
National origin France
Manufacturer Dassault Aviation
First flight 10 March 1978
Introduced June 1984
Primary users French Air Force
Indian Air Force
United Arab Emirates Air Force
Republic of China Air Force
Number built 611
Unit cost US$23 million
Developed from Dassault Mirage III
Variants Dassault Mirage 2000N/2000D
Dassault Mirage 4000

Development

The Avion de Combat Futur (ACF) (French: "Future combat aircraft") was developed for the French Air Force in the early 1970s. After the ACF was canceled on 18 December 1975 due to its growing cost and complexity, Dassault offered the Mirage 2000 as an alternative. This was a return to the first generation Mirages, but with several important innovations that tried to solve their shortcomings. Project chiefs were B.C. Valliéres, J.Cabrière, J.C. Veber and B.Revellin-Falcoz.[1]

Development of this small aircraft would also give the company a competitor to the General Dynamics F-16 Fighting Falcon, which had defeated the Dassault Mirage F1 in a contest for a new fighter for the air forces of Belgium, Denmark, Netherlands and Norway. Small single-engined fighters were clearly the most appreciated by foreign customers, as experience with the larger, twin-engined Mirage 4000 would show.

The prototype made its first flight in 10 March 1978 with test pilot Jean Coreau at the controls. Despite the new technologies applied, basing the new aircraft on the Mirage III allowed the development of a flyable prototype in only 27 months from the program start to the first flight, even if active service status needed another six years.

In that summer, at the Farnbourgh airshow, this machine displayed not only excellent handling capabilities, but also a full control at 204 km/h and 26 Angle of Attack. This was totally unexpected in a delta-wing fighter, and proof how CCD controls were capable of overcoming the delta wing shortcomings related to poor low-speed control, while retaining the advantages, such as low-drag, low radar cross section, ideal high speed aerodynamics and simplicity, provided by the absence of horizontal tail surfaces.[citation needed] The Mirage 2000 was one of the stars of that airshow and became the direct adversary for the F-16, which shared the CCD control and relaxed stability.[2] The 02 Prototype followed in 18 September 1978 and 03 in 26 September 1979. After 400 hours of flight, they were sent to CEV (Centre Experimental du Vol). The 04 Prototype was a demonstrator made by Dassault for its own purposes, and finally the first dual-seat M.2000B flew in 11 October 1980.

The first production example flew on 20 November, 1982 and the aircraft went into operational service in 1984. They were practically pre-production aircraft, because they had no SARH missiles (RDM-1 radar) and the first model of SNECMA 'Super Atar' M-53-2. The last Mirage 2000 was delivered on 23 November 2007.[3]

The Mirage 2000 is scheduled to be replaced in French service by the Dassault Rafale, which became operational with the French Air Force on 27 June 2006. The Mirage 2000 production line was shut down in November 2007 after the last aircraft had been delivered to the Hellenic Air Force.

[edit] Design

Using the concept of the delta wing interceptor seen on the Dassault Mirage III, Dassault built a new fighter jet design. This configuration is not ideal with regard to maneuverability, low-altitude flight, and distance required for take-off and landing, but has advantages in high-speed flight characteristics, simplicity of construction, low radar signature and internal volume.

[edit] Features

French Mirage 2000C fully armed.

The Mirage 2000 features a low-set thin delta wing with cambered section, 58 degrees leading-edge sweep (4 at the exit wing border) and moderately blended root; area-ruled; two small canard wings, fixed, placed just behind the air intakes. The flight commands on the wing are: four elevons (+15/-30°), four slats, four airbrakes (2 above and 2 below each wing).

Its neutral point is in front of its center of gravity, giving the fighter relaxed stability to enhance maneuverability. It was the first fighter jet to incorporate negative stability in its design.[4] An airbrake is fitted on top and below each wing in an arrangement very similar to that of the Mirage III. A noticeably taller tailfin allows the pilot to retain control at higher angles of attack, assisted by small strakes mounted along each air intake.

It has a runway arresting hook or fairing for a brake parachute can be fitted under the tail. The landing roll was reduced by robust carbon brakes. The backward-retracting, steerable nose gear features dual wheels, while the main gear features single wheels and retracts inward into the wings. A parachute brake is on the tail, just above the engine exhaust.

[edit] Structure

Multi-spar metal wing; elevons have carbon-fiber skins with AG5 light alloy honeycomb cores; carbon-fiber/light alloy honeycomb panel covers avionics bay; most of the tailfin and all of the rudder are skinned with boron/epoxy/carbon; the rudder has a light alloy honeycomb core.

Dassault Mirage 2000C at Paris Air Show 2007

[edit] Flight control system

The aircraft has a redundant fly-by-wire automatic flight control system, providing a high degree of agility and easier handling, together with stability and precise control in all situations. The fighter's airframe is naturally unstable, and so it is coupled with FBW commands to obtain the best agility; however, in override mode it is still possible to exceed a 270 deg/sec roll rate and allows the aircraft to reach 11 g (within the 12 g structural limit), instead of 9 g when engaged. The system is reliable with no known losses due to its failure.

[edit] Landing gear

The aircraft uses a retractable tricycle type landing gear by Messier-Bugatti, with twin nosewheels and a single wheel on each main gear. Hydraulic retraction, nosewheels rearward, main units inward. Oleo-pneumatic shock absorbers. Electrohydraulic nosewheel steering (+/-45 degrees). Manual disconnect permits the nosewheel unit to caster through 360 degrees for ground towing.

[edit] Cockpit

The fighter is available as a single-seat or two-seat multi-role fighter. The pilot flies the aircraft by means of a centre stick and left hand throttles, with both incorporating hands-on-throttle-and-stick (HOTAS) controls. The pilot sits on a SEMB Mark 10 zero-zero ejection seat (a license-built version of the British Martin-Baker Mark 10). Unlike in the F-16, the pilot sits in a conventional position, without the steep backward slope of the F-16 seat. The cockpit is quite small, and there is no bubble canopy. Despite this, the cockpit visibility is quite good, but less than the F-16, especially in the 'six o'clock' (rearwards-looking) position.

The instrument panel (in the Mirage 2000 C) is dominated by a Heads Up Display (HUD) with the VMC 180 radar screen located centrally below it. To the lower left is a stores management panel, above which are the navigation instruments and altimeter. The right half of the instrument panel accommodates the engine and systems displays. Located on the left side of the cockpit, just ahead of the throttle, are controls for the communications equipment, including the Have Quick secure radio.

[edit] Avionics

Standard avionics for the Mirage-2000B/C include:

  • Sagem ULISS 52 inertial navigation system (INS), TRT radio altimeter.
  • Sextant TMV-980 data display system (VE-130 head-up and VMC-180 head-down) (two head-down in 2000N/D). The combined head-up/head-level display is collimated at infinity, and presents data relating to flight control, navigation, target engagement and weapon firing. Sensor and system management data is presented on two colored lateral displays.
  • Dassault Electronique Type 2084 central digital computer, Digibus digital databus (2084 XR in 2000D) and Sextant Avionique Type 90 air data computer.
  • LMT NRAI-7A IFF transponder, IO-300-A marker beacon receiver, TRT ERA 7000 V/UHF com transceiver, TRT ERA 7200 UHF or EAS secure voice communications.

[edit] Radar

Thomson-CSF RDM multi-mode radar or Dassault Electronique/Thomson-CSF RDI pulse-Doppler radar for the Mirage 2000C/D, each with an operating range of 54 nm (100 km / 62 miles). This unit was an evolution of Cyrano radars, with more modern processing units and look-down/shoot-down capabilities. The effective range is around 60–70 km with modest capabilities against low-level targets. It is linked with Super R.530F missiles, and equipped the first 37 aircraft delivered to the French Air Force (Armée de l'Air) and most exported Mirages. It has multirole capabilities that enable its use in air-to-surface tasks, including anti-ship roles. The very early RDM were still not linked with the Super R.530F missiles, but it was solved quickly.

  • RDI interception radar. A specialized radar for air-to-air tasks delivered mainly with the Mirage 2000C for the Armée de l'Air. It has a much improved range of about 150 km, and is linked to Super R.530D missiles; much improved compared to the "F". Look-down/shoot-down capabilities are much improved as well, but this radar is not usually used for air-to-surface roles.
  • Dassault/Thales Antelope 5 Radar with terrain avoidance capability for Mirage 2000N Nuclear Strike variant.
  • The Thales multimode RDY (Radar Doppler Multitarget) developed for the Mirage 2000-5. Third generation radar, with multiple target capabilities (comparable to the AWG-9) and MICA missiles. This radar equipped many of the most recently exported M.2000s, as well as the first Mirage 2000RDM updated to 2000-5 standard.

[edit] Countermeasures

  • Thales Serval Radar warning receiver (RWR) with antennas on the wingtips and on the rear of the top of the tailfin.
  • Dassault Sabre RF jammer in a pod below the bottom of the tailfin, with an antenna in a fairing on the front of the tailfin.
  • Dassault Éclair dispenser system under the tail. This was eventually replaced by a pair of Matra Spirale dispensers, one fitted on an extension behind the rear of each wingroot, giving a total capacity of 224 cartridges.

[edit] Engines

The Mirage 2000 is equipped with a SNECMA M53-5 (first 37 airplanes), or SNECMA M53-P2 low-bypass ratio turbofan engine, depending on the aircraft version, which provides 64 kN of thrust dry and 98 kN in afterburner. The air intakes are fitted with an adjustable half-cone-shaped centerbody, which provides an inclined shock of air pressure for highly efficient air intake. Total internal fuel capacity is 3,978 litres in the Mirage 2000C and E, and 3,904 litres in the Mirage 2000B, N, D and S. There are also provisions for a jettisonable 1,300-litre centerline fuselage fuel tank and for a 1,700-litre drop tank under each wing.

[edit] Armament and payload

The Mirage 2000 is equipped with built-in twin DEFA 554 (now GIAT 30-550 F4) 30 mm revolver-type cannons with 125 rounds each. The cannons have selectable fire rates of 1,200 or 1,800 rounds per minute. Each round weigh 275 g and have a muzzle velocity of around 800 m/s.

The Mirage 2000 can carry up to 6.3 tonnes (13,900 lb) (or 7 tonnes for -9 version) of stores on nine pylons, with two pylons on each wing and five under the fuselage. External stores include:

  • Matra Super 530 medium-range semi-active radar-guided air-to-air missile on the inboard wing pylons and underbelly one.
  • MICA missiles are replacing the previous. They are available only on the Mirage 2000-5 and further models. They have multiple advantages over previous missiles such as their weight, only 110 kg compared to 250-270 kg. This allows the aircraft to carry up to 5 missiles under the belly. The data-link, active radar and auto-pilot make these weapons comparable to the heavier AMRAAM. The range is around 60 km, even more than the Super R.530D. So a Mirage 2000-5 with 4 MICA can engage four targets at the same time up to 60 km range, while a Mirage 2000 RDI can engage only two (not at the same time) within 40 km.
  • Matra Magic short-range infrared-seeking AAM on the outboard wing pylons. Other missiles are compatible, because Magic itself was meant as 'Sidewinder compatible', so AIM-9J/P/L are often used on exported Mirages, and often other IR missiles are also in the Mirages panoply.
  • The Mirage 2000C can carry air-to-ground stores such as the Matra 68 mm rocket pods (18 each), iron bombs (both French 250, 400, 1000 kg and Mk 80s series), and cluster bombs like Belouga or foreigner models. Some sub-version, especially those equipped with RDM (mainly used in export models) have the capability to use the Exocet anti-ship missiles.

A fixed removable refuelling probe can be attached in front of the cockpit, offset slightly to the right of center.

[edit] Operational history

French Mirage 2000s saw operational use during the Gulf War although little combat action. UAE Mirages also flew in the Gulf War, but saw little action.

French Mirage 2000s were prominent participants in UN and NATO air operations over the former Yugoslavia, with one aircraft shot down over Bosnia by a MANPADS heat-seeking surface-to-air missile fired by air defence units of Army of Republika Srpska during operation Deliberate Force in 1995, prompting efforts to obtain improved defensive systems.

On 8 October 1996[5], during the escalation over Imia/Kardak a Greek Mirage 2000 fired an R550 Magic 2 and shot down a Turkish F-16D (serial 91-0023) over the Aegean Sea, the only confirmed F-16 lost in air-to-air warfare. The pilot died, while the co-pilot ejected and was rescued by Greek forces.

AdA Mirage 2000Ds served in the intervention in Afghanistan in 2001-2002, operating in close conjunction with international forces and performing precision attacks with LGBs.

In summer 2007, after the Rafale fighters have been removed from the theater of operations, 3 French Mirage 2000's were deployed to Afghanistan in support of NATO troops.

Kargil War, 1999: India has assigned the nuclear strike role to their Mirage 2000s. In 1999 when the Kargil conflict broke out, the Mirage 2000 performed well during the whole conflict in the Himalayan peaks, even though the Mirages supplied to India had limited air interdiction capability and had to be heavily modified to drop dumb and laser-guided bombs. The two Mirage squadrons flew a total of 515 sorties, and in 240 strike missions dropped 55,000 kg of ordnance. Easy maintenance and a very high sortie rate made the Mirage 2000 one of the most efficient fighter of the Indian Air Force in the conflict.

[edit] Variants

[edit] Mirage 2000C

French Mirage 2000C

The first Mirage 2000 to go into service was the single-seat Mirage 2000C interceptor. There were four single-seat prototypes, including the initial Mirage 2000 prototype. The first production Mirage 2000C flew in November 1982. Deliveries began in 1983. The first operational squadron was formed in 1984, the 50th anniversary of the French Air Force. A total of 124 Mirage-2000Cs were obtained by the AdA.

The first 37 Mirage 2000Cs delivered were fitted with the Thomson-CSF RDM (Radar Doppler Multifunction) and were powered by the SNECMA M53-5 turbofan engine. The 38th Mirage 2000C had an upgraded SNECMA M53-5 P2 turbofan engine. The Radar Doppler Impulse (RDI) built by Thales did not enter service until 1987.

Latest upgrades include:

  • Non-Cooperative Target Recognition (NTCR) mode in RDI Radar allows identification of airborne targets not responding on IFF.
  • Integration with the new Matra MICA (Missile d'Interception, de Combat et d'Autodefense) IR heat-seeking missile. The radar-guided version of the MICA will not be able to support earlier versions of the Mirage 2000.
  • Indian Mirage-2000s have been integrated to carry the Russian R-73AE Archer missile and the indigenous Indian built Astra missile.

[edit] Mirage 2000B

Mirage 2000B nose close up.

The Mirage 2000B is two-seat operational conversion trainer variant which performed its initial flight on October 11, 1980. The AdA acquired 30 Mirage 2000Bs, with all three of the AdA fighter wings obtaining a few each for conversion training.

[edit] Mirage 2000N and 2000D

The Mirage 2000N is the nuclear strike variant which was intended to carry the Aerospatiale Air-Sol Moyenne Portee (ASMP) nuclear stand-off missile. Initial flight tests of two prototypes began on February 3, 1983, and the Mirage 2000N entered operational service in 1988. A total of 75 were built.

The Mirage 2000D is a dedicated conventional attack variant developed from the Mirage 2000N. Initial flight of the Mirage 2000D prototype, a modified Mirage 2000N prototype, was on February 19, 1991. The first flight of a production aircraft occurred March 31, 1993, and service introduction followed in April 1995. A total of 86 were built.

[edit] Mirage 2000-5

By the late 1980s, the Mirage 2000 was beginning to age compared with the latest models of U.S. F-16 fighters, so Thomson-CSF began work on a privately funded update of the Mirage 2000C which was to be named the Mirage 2000-5. A two-seat Mirage 2000B prototype was extensively modified as the first Mirage 2000-5 prototype, and it first flew on October 24, 1990. A Mirage 2000C prototype was then reworked to a similar standard, making its initial flight on April 27, 1991.

Features:

  • The Thales multimode RDY (Radar Doppler Multitarget). The RDY radar is the heart of the upgrade, providing true multitarget tracking. It can simultaneously detect up to 24 targets and track the eight highest-priority threats while guiding four MICA EMs to different targets simultaneously.
  • The updated ICMS 2 countermeasures suite and the Samir DDM missile warning system. ICMS 2 incorporates a receiver and associated signal processing system in the nose for detection of hostile missile command data links. The aircraft’s self-protection equipment can be interfaced to a new programmable mission-planning and post-mission analysis ground system.
  • A new glass cockpit layout borrowed from the Rafale program with three-color MFDs, a dual-linked wide-angle HUD / head-level display, and HOTAS controls. The cockpit is NVG-compatible.
  • Targeting systems included the Thales TV/CT CLDP laser designation pod which provides the capability to fire laser-guided weapons by day and night.
  • A two-seater version was developed as well. The back-seater has the HUD but not the associated head-level display, and as with first-generation two-seaters, there are no built-in cannon (although cannon pods can be carried).
  • The Mirage 2000-5 can also carry the oversized drop tanks developed for the Mirage 2000N, greatly extending its range.

In 1993, the AdA decided to upgrade 37 of their existing Mirage 2000s to the 2000-5 specification as a stopgap before the arrival of the Rafale in AdA service. The upgraded aircraft were redesignated Mirage 2000-5F, and became operational in 2000. They retained the old countermeasures system with the Serval/Sabre/Spirale units and did not receive the ICMS 2 system.

The AdA is now considering upgrades for the type, including the MIDS datalink, MICA IR support, and the Thales Topsight helmet-mounted display / sighting system.

[edit] Mirage 2000-5 Mark 2

Dassault extended the improvements of the Mirage 2000-5 a bit further with the Mirage 2000-5 Mark 2, which is an enhanced, fully multirole version of the Mirage 2000-5. It is currently the most advanced version of the Mirage 2000.

Features:

  • Thales RDY-2 radar. This radar system is similar in configuration to the original RDY, but features two new air-to-ground modes, including a high-resolution synthetic aperture radar (SAR) imaging mode with a moving target indicator (MTI) capability to provide an all-weather, day/night targeting capability. The radar features low-probability-of-intercept (LPI) operation, with the output pattern varying in a seemingly random pattern that prevents an adversary RWR from recognizing that it has been targeted.
  • The high-power Modular Data Processing Unit (MDPU) designed for the Rafale.
  • A new Thales Totem 3000 INS with ring-laser gyros and GPS capability, providing much greater accuracy, higher reliability, and shorter alignment time replaces the older ULISS 52 system. It works in conjunction with a terrain-following system.
  • An improved, classified ICMS 3 digital countermeasures suite.
  • An on-board oxygen generation system (OBOGS).
  • The cockpit was updated as well, retaining the same general layout but with larger color displays and other modernizations. The Thales Topsight helmet-mounted display / sighting system is offered as an option.
  • The Mirage 2000-5 Mark 2 includes a datalink for the targeting of MICA ER missiles and can carry the Damocles targeting pod.
  • Future Upgrades: Thales AIDA visual identification pod; technology used in the Rafale will be also integrated into the Mirage 2000, including infrared and optical sensors for IFF and targeting. It will be used by AdA Mirage 2000-5Fs. Further development of the second-generation type is expected to include a GPS receiver, MIDS datalink, and unspecified long-range sensors.
  • Topsight E helmet-mounted sight

[edit] Mirage 2000E

"Mirage 2000E" was a blanket designation for a series of export variants of the Mirage 2000. These aircraft were fitted the M53-P2 engine and an enhanced "RDM+" radar, and all can carry the day-only ATLIS II laser targeting pod.

[edit] Mirage 2000M (Egypt)

Egypt was the first foreign buyer, ordering 16 single-seat Mirage 2000M and four Mirage 2000BM trainers in late 1981, with deliveries beginning in 1986. The Egyptians also purchased ATLIS II pods and a wide range of appropriate munitions, including Magic and Super 530 AAMs, AS-30L laser-guided ASMs, and Armat anti-radiation missiles.

[edit] Mirage 2000H (India)

Indian Air Force Mirage 2000H.

India has acquired a total of 49 examples, including 42 single-seaters and 7 Mirage two-seaters. The IAF named the Mirage Vajra (Thunderbolt). India also purchased appropriate stores along with the fighters, including ATLIS II pods and laser-guided weapons.

  • Since India wanted the fighter quickly, the first part of an initial batch of 26 single-seaters and 4 two-seaters was shipped to the Indian Air Force (IAF) beginning in 1985 with the older M53-5 engines. These aircraft were given the designations of Mirage 2000H5 and Mirage 2000TH5.
  • The second part of this initial batch consisted of 10 more single-seaters with the M53-P2 engine, with these aircraft designated Mirage 2000H. All the first batch was reengined with the M53-P2, with the single-seaters re-designated "Mirage 2000H" and the two-seaters re-designated Mirage 2000TH.
  • A second batch of six Mirage 2000H single-seaters and three Mirage 2000TH two-seaters was shipped in 1987-1988.

Recent orders:

  • In 2004, the Indian government approved purchase of ten more Mirage 2000Hs, with these machines featuring improved avionics, particularly an upgraded RDM-7 radar.
  • The Mirage 2000-5 was a contender for a planned Indian Air Force 126 fighter aircraft procurement in which it was competing with the Mikoyan MiG-35, F-16 Fighting Falcon and JAS 39 Gripen. However, Dassault announced it had replaced the Mirage 2000 with the Rafale as the contender for the deal since the Mirage 2000 production line was to be closed.
  • India has announced a $1.9 billion program to arm 51 of its Mirage 2000 aircraft with the MBDA ASRAAM dogfighting missile beginning in 2007. Installation will require new radar, electronic warfare equipment, and updates to the cockpit and data bus. Pilot helmets will require addition of a helmet-mounted sight. These will be the first Mirage aircraft to carry the British missile and Dassault, Thales, and MBDA are to participate in the effort.[6]

[edit] Mirage 2000P (Peru)

Peru placed an order for 10 single-seat Mirage 2000Ps and 2 Mirage 2000DP trainers. The Peruvians ordered a set of munitions similar to that ordered by Egypt, along with ATLIS II targeting pods.

[edit] Mirage 2000-5EI (Taiwan, ROC)

ASTAC pod

In 1992, the Republic of China Air Force ordered 48 single-seat Mirage 2000-5EI interceptors and 12 Mirage 2000-5DI trainers, with introduction of the first squadron in 1997 and the last fighters delivered in 1999. The Taiwanese ordered a set of ASTAC electronic intelligence (ELINT) pods for their Mirages.

  • France announced in 1992 that it would offer Dassault Mirage 2000-5 fighters to Taiwan. The number of aircraft considered had been rumoured to be 120, but the deal was finalized as 60 aircraft (48 single-seat 2000-5EIs and 12 two-seat 2000-5DIs) on November 17 of the same year. This marks the first ROCAF purchase of French fighters since the arrival of 24 Dewoitine D.510C piston-engine monoplanes in 1937. The program was given the codename "Fei Lung" (Flying Dragon).
  • The ROCAF also obtained 960 MICA medium-range and 480 Magic II short-range air-to-air missiles from Matra. The former provides the Mirage with the BVR capability needed for its role as front-line interceptor. A number of centerline twin gun pods with DEFA 554 cannons were also acquired and fitted on the two-seaters, as they do not have an internal gun armament. Other support equipment, such as auxiliary fuel tanks, helmets, and G-suits, have also been procured.
  • The first batch of ROCAF Mirage 2000-5s, consisting of five aircraft, arrived at Hualien Harbor on the east coast of Taiwan by sea on 1997-05-06. After being unloaded, they were towed to Hualien AB, where they were unpacked and checked, and then flown to Hsinchu AB. Subsequent deliveries also followed the same procedure. The last ROCAF Mirage 2000-5 was delivered in an official ceremony on 1998-11-26.

All Mirage 2000-5s are operated by the 499th TFW at Hsinchu. The first unit to convert to the type, the 41st TFS, was commissioned on 1997-12-01. Subsequently the 42nd TFS was commissioned on 1998-11-26. The 499th TFW achieved the IOC (Initial Operational Capability) status on 2001-05-10, and the 48th TFS was commissioned on the same day.

On 2004-11-01, the 41st and 42nd TFSs were upgraded to the "Tactical Fighter Group" status, while the 48th TFS became the 48th Training Group, in the largest restructure undertaken by the ROCAF since 1999. At the same time, the original 11th TFG went into history. Each of the new TFG/TG is commanded by a Colonel, but the number of aircraft assigned is not much different from that for a Squadron. Although their official English designation is Tactical Fighter Group, the Chinese designation literally means Operations Group.

Weapon Testing & Exercises
  • On 1998-05-08, a two-seat DI fired one MICA missile and successfully hit a target drone 67 km away. It was the first launch of the said missile outside France. The second MICA live-firing exercise took place off the east coast of Taiwan on 2000-03-29, in which 2051 (right side image) fired a single MICA missile from its left inner pylon.
  • On 2004-07-21, two Mirage 2000-5s from the 2nd TFW landed on the wartime reserve runway located at the Jenteh section of Highway No. 1 as part of the annual Han Kuang No. 20 Exercise. Mirage 2000-5DI 2051, piloted by Maj. Wei-Kuang Chang and Lt. Col. Juei-Chi Duan, and 2054, piloted by Lt. Col. Bin-Fu Wu and Capt. Jien-Liang Chen, took off from their home base Hsinchu Air Base at 0540 hrs. 2051 landed on the highway at 0620 hrs, followed by 2054 at 0622 hrs. The two jets then taxied to the other end of the reserve runway to be refueled and re-armed with two Magic air-to-air missiles, respectively. At 0712 hrs, 2051 took off again and 2054 followed one minute later. Both landed at Hsinchu at 0736 hrs.

[edit] Mirage 2000-5EDA (Qatar)

In 1994, Qatar ordered nine single-seat Mirage 2000-5EDAs and three Mirage 2000-5DDA trainers, with initial deliveries starting in 1997.

[edit] Mirage 2000EAD/RAD (UAE)

In 1983, the UAE purchased 22 single-seat Mirage 2000EADs, 8 unique single-seat Mirage 2000RAD reconnaissance variants, and 6 Mirage 2000DAD trainers, for a total order of 36 machines. The order specified an Italian-made defensive avionics suite that delayed delivery of the first of these aircraft until 1989.

  • The Mirage 2000RAD reconnaissance variant does not have any built-in cameras or sensors, and the aircraft can still be operated in air combat or strike roles. The reconnaissance systems are implemented in pods, including the Thales "SLAR 2000" radar pod, Dassault "COR2" multi-camera pod with visible and infrared imaging capability, and the Dassault "AA-3-38 HAROLD" telescopic long-range optical camera pod. The UAE is the only nation operating such a specialized reconnaissance variant of the Mirage 2000 at this time.

[edit] Mirage 2000EG (Greece)

Greek Mirage 2000EG climbing.

Beginning in March 1985, Greece ordered 36 single-seat Mirage 2000EGs and 4 Mirage 2000BG two-seat trainers, as a part of the "Talos" modernization project.

  • They feature an ICMS 1 defensive countermeasures suite, which is an updated version of the standard Mirage 2000C countermeasures suite and is characterized by two small antennas near the top of the tailfin. These Mirage 2000s were later modified in the field to carry the Aerospatiale AM39 Exocet anti-ship missile.
  • In 2000, Greece ordered a batch of 25 Mirage 2000-5 Mk.2 fighters, which feature the SATURN secure radio. The order included 15 new-build aircraft and 10 upgrades of existing Greek Mirage 2000EGs. Apparently the Greek order does not include any upgrades of two-seaters.

[edit] Mirage 2000BR (Brazil)

Dassault competed for a Brazilian deal with the Mirage 2000BR, another variant of the Mirage 2000-9. Due to Brazilian budget problems, the competition has dragged on for years until it was suspended in February 2005.

  • In July 2005, however, Brazil agreed to purchase 12 ex-AdA Mirage 2000C aircraft.
  • First two Mirage 2000C and Mirage 2000B delivered to Brazilian Air Force(FAB) on September 4 2006 . Aircraft were delivered to 1º GDA in Anápolis, Goiás to replace Mirage IIIEBR/DBR. Aircraft will be named F-2000 in FAB service. On August 26 of 2008, the last 2 Mirages were delivered.

[edit] Mirage 2000-9

Mirage 2000-9 is the export variant of Mirage 2000-5 Mk.2.

  • The UAE was the launch customer, ordering 32 new-build aircraft, comprising 20 Mirage 2000-9 single-seaters and 12 Mirage 2000-9D two-seaters. Initial deliveries of the UAE Mirages began in the spring of 2003. A further 30 of Abu Dhabi's older Mirage 2000s will also be upgraded to Mirage 2000-9 standard.
  • The UAE's Mirage 2000-9s are well-equipped for the strike mission, since they are being provided with the Shehab laser targeting pod (a variant of the Damocles) and the Nahar navigation pod, complementing the air-to-ground modes of the RDY-2 radar. They are also equipped with a classified countermeasures system designated "IMEWS", which is comparable to the ICMS 3. The UAE is also obtaining the "Black Shaheen" cruise missile, which is basically a variant of the MBDA Apache cruise missile similar to Storm Shadow.
  • On 4 April 2005, a Mirage 2000-9 crashed after take-off from Istres AB in southern France during a test flight before its delivery to Abu Dhabi. The two pilots, Dassault chief test pilot and a pilot from UAE, ejected safely and remained unhurt. An engine failure during take-off was the cause. The aircraft crashed over a deserted part of the airbase.[7].


Download Paper Model : Click Here