Wednesday, February 3, 2016

McDonnell Douglas F/A-18 Hornet

F/A-18 Hornet Papercraft AMERYKANSKI SAMOLOT WIELOZADANIOWY F/A-18 Hornet Papercraft McDonnell Douglas F/A-18 Hornet

The McDonnell Douglas (now Boeing) F/A-18 Hornet is a twin-engine supersonic, all-weather carrier-capable multirole combat jet, designed as both a fighter and attack aircraft (F/A designation for Fighter/Attack). Designed by McDonnell Douglas and Northrop, the F/A-18 was derived from the latter's YF-17 in the 1970s for use by the United States Navy and Marine Corps. The Hornet is also used by the air forces of several other nations. The U.S. Navy's Flight Demonstration Squadron, the Blue Angels, has used the Hornet since 1986.
The F/A-18 has a top speed of Mach 1.8 (1,034 knots, 1,190 mph or 1,915 km/h at 40,000 ft or 12,190 m). It can carry a wide variety of bombs and missiles, including air-to-air and air-to-ground, supplemented by the 20 mm M61 Vulcan cannon. It is powered by two General Electric F404 turbofan engines, which give the aircraft a high thrust-to-weight ratio. The F/A-18 has excellent aerodynamic characteristics, primarily attributed to its leading edge extensions (LEX). The fighter's primary missions are fighter escort, fleet air defense, Suppression of Enemy Air Defenses (SEAD), air interdiction, close air support and aerial reconnaissance. Its versatility and reliability have proven it to be a valuable carrier asset, though it has been criticized for its lack of range and payload compared to its earlier contemporaries, such as the Grumman F-14 Tomcat in the fighter and strike fighter role, and the Grumman A-6 Intruder and LTV A-7 Corsair II in the attack role.
The Hornet saw its first combat action in 1986 during the 1986 United States bombing of Libya and subsequently participated in 1991 Gulf War and 2003 Iraq War. The F/A-18 Hornet provided the baseline design for the Boeing F/A-18E/F Super Hornet, a larger, evolutionary redesign of the F/A-18.

Tuesday, November 25, 2014

Mitsubishi A6M3 Zero Papacraft Model

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The Mitsubishi A6M Zero was a long-range fighter aircraft, manufactured by Mitsubishi Heavy Industries, and operated by the Imperial Japanese Navy from 1940 to 1945. The A6M was designated as the Mitsubishi Navy Type 0 Carrier Fighter (零式艦上戦闘機 rei-shiki-kanjō-sentōki?), and also designated as the Mitsubishi A6M Rei-sen and Mitsubishi Navy 12-shi Carrier Fighter. The A6M was usually referred to by its pilots as the "Reisen" (zero fighter), "0" being the last digit of the Imperial year 2600 (1940) when it entered service with the Imperial Navy. The official Allied reporting name was "Zeke", although the use of the name "Zero" was later commonly adopted by the Allies as well.
When it was introduced early in World War II, the Zero was considered the most capable carrier-based fighter in the world, combining excellent maneuverability and very long range.[1] In early combat operations, the Zero gained a legendary reputation as a dogfighter, achieving the outstanding kill ratio of 12 to 1,[2] but by mid-1942 a combination of new tactics and the introduction of better equipment enabled the Allied pilots to engage the Zero on generally equal terms.[3]
The Imperial Japanese Navy Air Service ("IJNAS") also frequently used the type as a land-based fighter. By 1943, inherent design weaknesses and the failure to develop more powerful aircraft engines meant that the Zero became less effective against newer enemy fighters, which possessed greater firepower, armor, and speed, and approached the Zero's maneuverability. Although the Mitsubishi A6M was outdated by 1944, design delays and production difficulties of newer Japanese aircraft types meant that it continued to serve in a front line role until the end of the war. During the final years of the War in the Pacific, the Zero was also adapted for use in kamikaze operations.[4] During the course of the war, Japan produced more Zeros than any other model of combat aircraft.[5]



A6M "Zero"
A6M3 Zero N712Z 1.jpg
Mitsubishi A6M3 Zero Model 22 (NX712Z), recovered from New Guinea in 1991 and used in the film Pearl Harbor
Role Fighter
Manufacturer Mitsubishi Heavy Industries, Ltd
Designer Jiro Horikoshi
(chief designer)
First flight 1 April 1939
Introduction 1 July 1940
Retired 1945 (Japan)
Primary users Imperial Japanese Navy Air Service
Chinese Nationalist Air Force
Produced 1940–1945
Number built 10,939
Variants Nakajima A6M2-N













Design and development


Mitsubishi A6M3 Zero wreck abandoned at Munda Airfield, Central Solomons, 1943

A6M2 Zero photo c. 2004

Carrier A6M2 and A6M3 Zeros from the aircraft carrier Zuikaku preparing for a mission at Rabaul

A6M3 Model 22, flown by Japanese ace Hiroyoshi Nishizawa over the Solomon Islands, 1943
The Mitsubishi A5M fighter was just entering service in early 1937, when the Imperial Japanese Navy started looking for its eventual replacement. In May, they issued specification 12-Shi for a new carrier-based fighter, sending it to Nakajima and Mitsubishi. Both firms started preliminary design work while they awaited more definitive requirements to be handed over in a few months.
Based on the experiences of the A5M in China, the Imperial Japanese Navy sent out updated requirements in October calling for a speed of 600 km/h (370 mph) and a climb to 3,000 m (9,800 ft) in 3.5 min. With drop tanks, they wanted an endurance of two hours at normal power, or six to eight hours at economical cruising speed. Armament was to consist of two 20 mm cannons, two 7.7 mm (.303 in) machine guns and two 30 kg (66 lb) or 60 kg (132 lb) bombs. A complete radio set was to be mounted in all aircraft, along with a radio direction finder for long-range navigation. The maneuverability was to be at least equal to that of the A5M, while the wingspan had to be less than 12 m (39 ft) to allow for use on an aircraft carrier. All this was to be achieved with available engines, a significant design limitation. The Zero's powerplant seldom reached 750 kilowatts (about 1,000 hp) in any of its variants.
Nakajima's team considered the new requirements unachievable and pulled out of the competition in January. Mitsubishi's chief designer, Jiro Horikoshi, felt that the requirements could be met, but only if the aircraft could be made as light as possible. Every possible weight-saving measure was incorporated into the design. Most of the aircraft was built of a new top-secret 7075 aluminium alloy developed by Sumitomo Metal Industries in 1936. Called Extra Super Duralumin (ESD), it was lighter and stronger than other alloys (e.g. 24S alloy) used at the time, but was more brittle and prone to corrosion[6] which was countered with an anti-corrosion coating applied after fabrication. No armor was provided for the pilot, engine or other critical points of the aircraft, and self-sealing fuel tanks, which were becoming common at the time, were not used. This made the Zero lighter, more maneuverable, and the longest range single engine fighter of WWII; which made it capable of searching out an enemy hundreds of miles away, bringing them to battle, then returning hundreds of miles back to its base or aircraft carrier. However, that trade in weight and construction also made it prone to catching fire and exploding when struck by enemy rounds.[7]
With its low-wing cantilever monoplane layout, retractable, wide-set landing gear and enclosed cockpit, the Zero was one of the most modern aircraft in the world at the time of its introduction. It had a fairly high-lift, low-speed wing with a very low wing loading. This, combined with its light weight, resulted in a very low stalling speed of well below 60 kn (110 km/h; 69 mph). This was the main reason for its phenomenal maneuverability, allowing it to out-turn any Allied fighter of the time. Early models were fitted with servo tabs on the ailerons after pilots complained control forces became too heavy at speeds above 300 kilometres per hour (190 mph). They were discontinued on later models after it was found that the lightened control forces were causing pilots to overstress the wings during vigorous maneuvers.[8]
It has been claimed that the Zero's design showed clear influence from American fighter planes and components exported to Japan in the 1930s, and in particular the Vought V-143 fighter. Chance Vought had sold the prototype for this aircraft and its plans to Japan in 1937. Eugene Wilson, President of Vought, claimed that when shown a captured Zero in 1943, he found that "There on the floor was the Vought V 142 [sic] or just the spitting image of it, Japanese-made," while the "power-plant installation was distinctly Chance Vought, the wheel stowage into the wing roots came from Northrop, and the Japanese designers had even copied the Navy inspection stamp from Pratt & Whitney type parts."[9] While the sale of the V-143 was fully legal,[9][10] Wilson later acknowledged the conflicts of interest that can arise whenever military technology is exported.[9] In fact, there was no significant relationship between the V-143 (which was an unsuccessful design that had been rejected by the U.S. Army Air Corps and several export customers) and the Zero, with only a superficial similarity in layout. Allegations about the Zero being a copy have been mostly discredited.[10][11]

Name

The A6M is universally known as the "Zero" from its Japanese Navy type designation, Type 0 Carrier Fighter (Rei shiki Kanjō sentōki, 零式艦上戦闘機), taken from the last digit of the Imperial year 2600 (1940), when it entered service. In Japan, it was unofficially referred to as both Rei-sen and Zero-sen; Japanese pilots most commonly called it Zero-sen, where sen is the first syllable of sentoki, Japanese for "fighter."[N 1] [12]
In the official designation "A6M" the "A" signified a carrier-based fighter, "6" meant it was the sixth such model built for the Imperial Navy, and "M" indicated the manufacturer, Mitsubishi.
The official Allied code name was "Zeke", in keeping with the practice of giving male names to Japanese fighters, female names to bombers, bird names to gliders, and tree names to trainers. "Zeke" was part of the first batch of "hillbilly" code names assigned by Captain Frank T. McCoy of Tennessee, who wanted quick, distinctive, easy-to-remember names. When, in 1942, the Allied code for Japanese aircraft was introduced, he logically chose "Zeke" for the "Zero." Later, two variants of the fighter received their own code names: the Nakajima A6M2-N (floatplane version of the Zero) was called "Rufe" and the A6M3-32 variant was initially called "Hap". After objections from General "Hap" Arnold, commander of the USAAF, the name was changed to "Hamp". When captured examples were examined in New Guinea, it was realized it was a variant of the Zero and finally renamed "Zeke 32."

Operational history


Mitsubishi A6M2 "Zero" Model 21 takes off from the aircraft carrier Akagi, to attack Pearl Harbor.

Cockpit (starboard console) of a damaged A6M2 which crashed into Building 52 at Fort Kamehameha, Oahu, during the 7 December 1941 raid on Pearl Harbor. The pilot, who was killed, was NAP1/c Takeshi Hirano; aircraft's tail code was "AI-154", assigned to Akagi.

The Akutan Zero is inspected by US military personnel on Akutan Island on 11 July 1942.
The first Zeros (pre-series A6M2) went into operation in July 1940.[13] On 13 September 1940, the Zeros scored their first air-to-air victories when 13 A6M2s led by Lieutenant Saburo Shindo attacked 27 Soviet-built Polikarpov I-15s and I-16s of the Chinese Nationalist Air Force, shooting down all the fighters without loss to themselves. By the time they were redeployed a year later, the Zeros had shot down 99 Chinese aircraft[14] (266 according to other sources).[13]
At the time of the attack on Pearl Harbor 420 Zeros were active in the Pacific. The carrier-borne Model 21 was the type encountered by the Americans. Its tremendous range of over 2,600 km (1,600 mi) allowed it to range farther from its carrier than expected, appearing over distant battlefronts and giving Allied commanders the impression that there were several times as many Zeros as actually existed.[15]
The Zero quickly gained a fearsome reputation. Thanks to a combination of excellent maneuverability and firepower, it easily disposed of the motley collection of Allied aircraft sent against it in the Pacific in 1941. It proved a difficult opponent even for the Supermarine Spitfire. Although not as fast as the British fighter, the Mitsubishi fighter could out-turn the Spitfire with ease, could sustain a climb at a very steep angle, and could stay in the air for three times as long.[16]
Soon, however, Allied pilots developed tactics to cope with the Zero. Due to its extreme agility, engaging a Zero in a traditional, turning dogfight was likely to be fatal. It was better to roar down from above in a high-speed pass, fire a quick burst, then climb quickly back up to altitude. (A short burst of fire from heavy machine guns or cannon was often enough to bring down the fragile Zero.) Such "boom-and-zoom" tactics were used successfully in the China Burma India Theater (CBI) by the "Flying Tigers" of the American Volunteer Group (AVG) against similarly maneuverable Japanese Army aircraft such as the Nakajima Ki-27 Nate and Ki-43 Oscar. AVG pilots were trained to exploit the advantages of their P-40s, which were very sturdy, heavily armed, generally faster in a dive and level flight at low altitude, with a good rate of roll.[17]
Another important maneuver was Lieutenant Commander John S. "Jimmy" Thach's "Thach Weave", in which two fighters would fly about 60 m (200 ft) apart. If a Zero latched onto the tail of one of the fighters, the two aircraft would turn toward each other. If the Zero followed his original target through the turn, he would come into a position to be fired on by the target's wingman. This tactic was first used to good effect during the Battle of Midway, and later over the Solomon Islands. Many highly experienced Japanese aviators were lost in combat, resulting in a progressive decline in the quality of the opponents faced by Allied pilots, which became a significant factor in Allied successes. Unexpected heavy losses of these pilots at the battles of the Coral Sea and Midway dealt the Japanese carrier air force a blow from which it never fully recovered.[18][19]
However, throughout the engagement at Midway, the Allied Pilots registered a high dissatisfaction with the current state of the Grumman F4F Wildcat. The Commanding Officer of the USS Yorktown noted:
The fighter pilots are very disappointed with the performance and length of sustained fire power of the F4F-4 airplanes. The Zero fighters could easily outmaneuver and out-climb the F4F-3, and the consensus of fighter pilot opinion is that the F4F-4 is even more sluggish and slow than the F4F-3. It is also felt that it was a mistake to put 6 guns on the F4F-4 and thus to reduce the rounds per gun. Many of our fighters ran out of ammunition even before the Jap dive bombers arrived over our forces; these were experienced pilots, not novices.[20]
They were astounded by the Zero's superiority:
In the Coral Sea, they made all their approaches from the rear or high side and did relatively little damage because of our armor. It also is desired to call attention to the fact that there was an absence of the fancy stunting during pull outs or approaches for attacks. In this battle, the Japs dove in, made the attack and then immediately pulled out, taking advantage of their superior climb and maneuverability. In attacking fighters, the Zeros usually attacked from above rear at high speed and recovered by climbing vertically until they lost some speed and then pulled on through to complete a small loop of high wing over which placed them out of reach and in position for another attack. By reversing the turn sharply after each attack the leader may get a shot at the enemy while he is climbing away or head on into a scissor if the Jap turns to meet it.[20]
In contrast, Allied fighters were designed with ruggedness and pilot protection in mind.[21] The Japanese ace Saburō Sakai described how the resilience of early Grumman aircraft was a factor in preventing the Zero from attaining total domination:
I had full confidence in my ability to destroy the Grumman and decided to finish off the enemy fighter with only my 7.7 mm machine guns. I turned the 20mm cannon switch to the 'off' position, and closed in. For some strange reason, even after I had poured about five or six hundred rounds of ammunition directly into the Grumman, the airplane did not fall, but kept on flying! I thought this very odd—it had never happened before—and closed the distance between the two airplanes until I could almost reach out and touch the Grumman. To my surprise, the Grumman's rudder and tail were torn to shreds, looking like an old torn piece of rag. With his plane in such condition, no wonder the pilot was unable to continue fighting! A Zero which had taken that many bullets would have been a ball of fire by now.[22]
When the powerful Lockheed P-38 Lightning, Grumman F6F Hellcat and Vought F4U Corsair appeared in the Pacific theater, the A6M, with its low-powered engine, was hard-pressed to remain competitive. In combat with an F6F or F4U, the only positive thing that could be said of the Zero at this stage of the war was that in the hands of a skillful pilot it could maneuver as well as most of its opponents.[15] Nonetheless, in competent hands the Zero could still be deadly.
Due to shortages of high-powered aviation engines and problems with planned successor models, the Zero remained in production until 1945, with over 11,000 of all variants produced.

Allied opinions

File:Recognition of the Japanese Zero Fighter.ogvPlay media
Recognition of the Japanese Zero Fighter (1943)
The American military discovered many of the A6M's unique attributes when they recovered a largely intact specimen, the Akutan Zero, on Akutan Island in the Aleutians. During an air raid over Dutch Harbor on 4 June 1942, one A6M fighter was hit by ground fire. Losing oil, Flight Petty Officer Tadayoshi Koga attempted an emergency landing on Akutan Island about 20 miles northeast of Dutch Harbor, but his Zero flipped over in soft ground in a sudden crash landing. Koga died instantly of head injuries, but the relatively undamaged fighter was found over a month later by an American salvage team and shipped to Naval Air Station North Island where testing flights of the repaired A6M revealed both strengths and deficiencies in design and performance.[21][23]
The experts who evaluated the captured Zero found that the plane weighed about 2,360 kg (5,200 pounds) fully loaded, about half the weight of the standard United States Navy fighter. It was "built like a fine watch"; the Zero was constructed with flush rivets, and even the guns were flush with the wings. The instrument panel was a "marvel of simplicity ... with no superfluities to distract [the pilot]." What most impressed the experts was that the Zero's fuselage and wings were constructed in one piece, unlike the American method that built them separately and joined the two parts together. The Japanese method was much slower, but resulted in a very strong structure and improved close maneuverability.[21]
Captain Eric Brown, the Chief Naval Test Pilot of the Royal Navy, recalled being impressed by the Zero during tests of captured aircraft. "I don’t think I have ever flown a fighter that could match the rate of turn of the Zero. The Zero had ruled the roost totally and was the finest fighter in the world until mid-1943."[2] American test pilots found that the Zero's controls were "very light" at 320 kilometres per hour (200 mph), but stiffened at faster speeds (above 348 km/h, or 216 mph) to safeguard against wing failure.[24] The Zero could not keep up with Allied aircraft in high speed maneuvers, and its low "never exceed speed" (VNE) made it vulnerable in a dive. While stable on the ground despite its light weight, the aircraft was designed purely for the attack role, emphasizing long range, maneuverability, and firepower at the expense of protection of its pilot. Most lacked self-sealing tanks and armor plating.[21]

Variants

Type zero fighter en-hierarchy.png

A6M1, Type 0 Prototypes

The first A6M1 prototype was completed in March 1939, powered by the 580 kW (780 hp) Mitsubishi Zuisei 13 engine with a two-blade propeller. It first flew on 1 April, and passed testing in a remarkably short period of time. By September, it had already been accepted for Navy testing as the A6M1 Type 0 Carrier Fighter, with the only notable change being a switch to a three-bladed propeller to cure a vibration problem.

A6M2 Type 0 Model 11

While the Navy was testing the first two prototypes, they suggested that the third be fitted with the 700 kW (940 hp) Nakajima Sakae 12 engine instead. Mitsubishi had its own engine of this class in the form of the Kinsei, so they were somewhat reluctant to use the Sakae. Nevertheless, when the first A6M2 was completed in January 1940, the Sakae's extra power pushed the performance of the Zero well past the original specifications.
The new version was so promising that the Navy had 15 built and shipped to China before they had completed testing. They arrived in Manchuria in July 1940, and first saw combat over Chungking in August. There they proved to be completely untouchable by the Polikarpov I-16s and I-153s that had been such a problem for the A5Ms currently in service. In one encounter, 13 Zeros shot down 27 I-15s and I-16s in under three minutes without loss. After hearing of these reports the Navy immediately ordered the A6M2 into production as the Type 0 Carrier Fighter, Model 11. Reports of the Zero's performance filtered back to the US slowly. There they were dismissed by most military officials, who felt it was impossible for the Japanese to build such an aircraft.

A6M2 Type 0 Model 21


A6M2 "Zero" Model 21 of Shokaku prior to attack on Pearl Harbor, 7 December 1941.
After the delivery of only 65 aircraft by November 1940, a further change was worked into the production lines, which introduced folding wingtips to allow them to fit on aircraft carriers. The resulting Model 21 would become one of the most produced versions early in the war. A feature was the improved range with 520lt wing tank and 320lt drop tank. When the lines switched to updated models, 740 Model 21s had been completed by Mitsubishi, and another 800 by Nakajima. Two other versions of the Model 21 were built in small numbers, the Nakajima-built A6M2-N "Rufe" floatplane (based on the Model 11 with a slightly modified tail), and the A6M2-K two-seat trainer of which a total of 508 were built by Hitachi and the Sasebo Naval Air Arsenal.[25]

A6M3 Type 0 Model 32


A6M3 Model 32.
In 1941, Nakajima introduced the Sakae 21 engine, which used a two-speed supercharger for better altitude performance, and increased power to 840 kW (1,130 hp). A prototype Zero with the new engine was first flown on July 15, 1941.[26]
The new Sakae was slightly heavier and somewhat longer due to the larger supercharger, which moved the center of gravity too far forward on the existing airframe. To correct for this, the engine mountings were cut back by 185 mm to move the engine toward the cockpit. This had the side effect of reducing the size of the main fuselage fuel tank (located between the engine and the cockpit) from 518 L (137 US gal) to 470 L (120 US gal). The cowling was redesigned to enlarge the cowl flaps, revise the oil cooler air intake, and move the carburetor air intake to the upper half of the cowling.[27]
The wings were redesigned to reduce span, eliminate the folding tips, and square off the wingtips. The inboard edge of the aileron was moved outboard by one rib, and the wing fuel tanks were enlarged accordingly to 420 L. The two 20 mm wing cannon were upgraded from the 99 Shiki 1 Gou Koteijū 1 Kata Kai 1 to the 99 Shiki 1 Gou Koteijū 3 Gata,[28] which required a bulge in the sheet metal of the wing below each cannon. The wings also included larger ammunition boxes, allowing for 100 rounds for each of the 20 mm cannon.
The Sakae 21 engine and other changes increased maximum speed by only 11 kph compared to the Model 21, but sacrifed nearly 1,000 km of range.[29] Nevertheless, the navy accepted the type and it entered production in April 1942.[30]
The shorter wing span led to better roll, and the reduced drag allowed the diving speed to be increased to 670 km/h (420 mph). On the downside, turning and range, which were the strengths of the Model 21, suffered due to smaller ailerons, decreased lift and greater fuel consumption. The shorter range proved a significant limitation during the Solomons Campaign, during which Zeros based at Rabaul had to travel nearly to their maximum range to reach Guadalcanal and return.[31] Consequently, the Model 32 was unsuited to that campaign[30] and was used mainly for shorter range offensive missions and interception.
The redesign was enough to prompt the US to assign the Model 32 a new code name, "Hap". This name was short-lived, as a protest from USAAF Commanding General Henry "Hap" Arnold forced a change to "Hamp". Soon after, it was realized that it was simply a new model of the "Zeke".
This variant was flown by only a small number of units, and only 343 were built.

A6M3 Type 0 Model 22

In order to correct the deficiencies of the Model 32, a new version with the folding wingtips of the Model 21, new fuel tanks in the outer wings, and attachments and fuel lines for a 330 L (90 US gal) drop tank under each wing were introduced. The internal fuel was increased to 570 L (137 US gal) in this model, regaining all of the range lost in the Model 32 variant.
As the wing had significant redesign, this version received a new navy designation, 22 型 (2-2 kata, known in the West as a Model 22). The new model entered service circa December 1942 (before the navy formally accepted the new design) and 560 were eventually produced, all by Mitsubishi.[32] This wing is seen with two armament configurations. The Model 22 has the same wing armament as in the Model 32.[32] The 22型甲 (2-2 kata kou, aka Model 22a) has one 99式2号固定銃3型 (9-9 shiki 2 gou koteijū 3 gata) cannon in each wing.[32] The barrel protrudes.
According to one theory, very late production Model 22s may have had a wing similar to the shortened, rounded-tip wing of the Model 52.[33] One such plane was photographed at Lakunai Airfield ("Rabaul East") in the second half of 1943, and the photo has been published in a number of Japanese books, e.g., Aero Detail 7 and 世界の傑作機 9 at page 33 (Sekai no Kessaku Ki, aka Famous Airplanes of the World 9, 1993). Although jumping to the conclusion that the cowling is that of the Models 32 and 22, the latter book proposes that the plane is an early production Model 52, based upon an unspecified manual (see below).[34] There is a growing body of evidence that this "hybrid" type is simply an early production Model 52 (see below). (The Model 32, 22, 22 kou, 52, 52 kou and 52 otsu were all powered by the Nakajima 栄 (Sakae) 21型 engine.[31] That engine kept its designation in spite of changes in the exhaust system for the Model 52.)

A6M4 Type 0 Model 41/42

Mitsubishi is unable to state with certainty that it ever used the designation "A6M4" or model numbers for it. However, "A6M4" does appear in a translation of a captured Japanese memo from a Naval Air Technical Arsenal, titled Quarterly Report on Research Experiments, dated 1 October 1942.[35] It mentions a "cross-section of the A6M4 intercooler" then being designed. Some researchers believe "A6M4" was applied to one or two prototype planes fitted with an experimental turbo-supercharged Sakae engine designed for high altitude.[36] Mitsubishi's involvement in the project was probably quite limited or nil; the unmodified Sakae engine was made by Nakajima.[31] The design and testing of the turbo-supercharger was the responsibility of the 第一海軍航空廠 (Dai Ichi Kaigun Kōkūshō, First Naval Air [Technical] Arsenal) at Yokosuka.[37] At least one photo of a prototype plane exists. It shows a turbo unit mounted in the forward left fuselage.
Lack of suitable alloys for use in the manufacture of a turbo-supercharger and its related ducting caused numerous ruptures, resulting in fires and poor performance. Consequently, further development of a turbo-supercharged A6M was cancelled. The lack of acceptance by the navy suggests that the navy did not bestow model number 41 or 42 formally, although it appears that the arsenal did use the designation "A6M4". The prototype engines nevertheless provided useful experience for future engine designs.[38]

A6M5 Type 0 Model 52


Mitsubishi A6M "Rei-Sen" (Zeke) captured in flying condition and test flown by the US's Technical Air Intelligence Center (TAIC).

Mitsubishi A6M5 Model 52s abandoned by the Japanese at the end of the war (Atsugi Naval air base) and captured by US forces.

A6M5c Zeros preparing to take part in a kamikaze attack in early 1945
Sometimes considered the most effective variant,[39] the Model 52 was developed to again shorten the wings to increase speed and dispense with the folding wing mechanism. In addition, ailerons, aileron trim tab and flaps were revised.[40] Produced first by Mitsubishi, most Model 52s were made by Nakajima. The prototype was made in June 1943 by modifying an A6M3 and was first flown in August 1943.[41] The first Model 52 is said in the handling manual[42] to have 製造番号 (seizō bangō, manufacture number) 3904,[43] which apparently refers to the prototype.
Research by Mr. Bunzo Komine published by Mr. Kenji Miyazaki states that aircraft 3904 through 4103 had the same exhaust system and cowl flaps as on the Model 22.[44] This is partially corroborated by two wrecks researched by Mr. Stan Gajda and Mr. L. G. Halls, seizō bangō 4007 and 4043, respectively.[45][46][47] (The upper cowling was slightly redesigned from that of the Model 22.[48])
A new exhaust system provided an increment of thrust by aiming the stacks aft and distributing them around the forward fuselage. The new exhaust system required "notched" cowl flaps and heat shields just aft of the stacks. (Note, however, that the handling manual translation states that the new style of exhaust commenced with number 3904. Whether this is correct, indicates retrofitting intentions, refers to the prototype but not to all subsequent planes, or is in error is not clear.) From seizō bangō 4274, the wing fuel tanks received carbon dioxide fire extinguishers.[49][50] From number 4354, the radio became the Model 3, aerial Mark 1, and at that point it is said the antenna mast was shortened slightly.[51] Through seizō bangō 4550, the lowest exhaust stacks were approximately the same length as those immediately above them. This caused hot exhaust to burn the forward edge of the landing gear doors and heat the tires. Therefore, from number 4551 Mitsubishi began to install shorter bottom stacks.[52] Nakajima manufactured the Model 52 at its Koizumi plant in Gunma Prefecture. [53] The A6M5 had a maximum speed of 565 km/h (351 mph) at 6,000 meters and reached that altitude in 7:01 minutes.[54]
Subsequent variants included:
  • A6M5a, Model 52甲 (Kō, a) - Starting at Mitsubishi number 4651, an armament change substituted the Type 99-2 Mark 4 cannon, a belt-fed gun of 125 rounds per gun, in place of the drum-fed Type 99-2 Mark 3 of 100 rpg. The larger bulge in the underside of the wing for each cannon was deleted and the ejection port for spent cartridge cases was moved. Thicker wing skinning was installed to permit higher diving speeds.[55]
  • A6M5b, Model 52乙 (Otsu, b) - Armament change: The 7.7 mm (.303 in) Type 97 gun (750 m/s muzzle velocity and 600 m/1,970 ft range) in the right forward fuselage was replaced by a 13.2 mm Type 3 Browning-derived gun (790 m/s muzzle velocity and 900 m/2,950 ft range) with 240 rounds. The larger weapon required an enlarged opening, creating a distinctive asymmetric appearance to the top of the cowling, and a revised gas outlet near the windscreen. In addition, each wing cannon received a fairing at the wing leading edge. A plate of armored glass 45 mm thick was fitted to the windscreen. A larger propeller spinner was fitted, suggesting a change to the propeller.[56] The central drop tank became one with fins, suspended on a slanted pipe. The first of this variant was completed in April 1944 and it was produced until October 1944.[57]
  • A6M5c, Model 52丙 (Hei, c) - Armament change: One 13.2 mm (.51 in) Type 3 machine gun with a rate of fire of 800 rpm was added in each wing outboard of the cannon, but the 7.7 mm gun at the left side of the cowl was deleted. Four racks for rockets or small bombs were installed outboard of the 13 mm gun in each wing. Engine change: Some sources state that the hei had a Sakae 31 engine[58] In addition, a 55 mm thick piece of armored glass was installed at the headrest and a plate of armor was installed behind the seat. The mounting of the central 300L drop tank changed to a four-post design.[59] Wing skin was thickened further. The first of this variant was completed in September 1944.[60] Because of the gain in weight, this variant was used mainly for intercepting B-29s and special attack.[61]
  • A6M5-S (A6M5 Yakan Sentōki) - Armament change: To intercept B-29s and other night-flying aircraft, an air arsenal converted some Model 52s to night fighters.[62] They were armed with one 20 mm Type 99 cannon behind the pilot, aimed upward and similar to the Luftwaffe Schräge Musik installation.[63] However, lack of radar prevented them from being very effective.
Some Model 21 and 52 aircraft were converted to "bakusen" (fighter-bombers) by hanging a bomb rack and 250 kg bomb in place of the centerline drop tank.
Perhaps seven[64] Model 52 planes were ostensibly converted into A6M5-K two-seat trainers; mass production was contemplated by Hitachi but not undertaken.[65]

A6M6c Type 0 Model 53c

This was similar to the A6M5c, but with self-sealing wing tanks and a Nakajima Sakae 31a engine featuring water-methanol engine boost.

A6M7 Type 0 Model 62

Similar to the A6M6 but intended for attack or Kamikaze role.

A6M8 Type 0 Model 64

Similar to the A6M6 but with the Sakae (now out of production) replaced by the Mitsubishi Kinsei 62 engine with 1,560 hp (1,164 kW), 60% more powerful than the engine of the A6M2.[13] This resulted in an extensively modified cowling and nose for the aircraft. The carburetor intake was much larger, a long duct like that on the Nakajima B6N Tenzan was added, and a large spinner—like that on the Yokosuka D4Y Suisei with the Kinsei 62—was mounted. The larger cowling meant deletion of the fuselage-mounted machine gun, but armament was otherwise unchanged from the Model 52 Hei (2 x 20 mm cannon; 2 x 13 mm/.51 in MG). In addition, the Model 64 was modified to carry two 150 L (40 US gal) drop tanks on either wing in order to permit the mounting of a 250 kg (550 lb) bomb on the underside of the fuselage. Two prototypes were completed in April 1945 but the chaotic situation of Japanese industry and the end of the war obstructed the start of the ambitious program of production for 6,300 machines, none being completed.[13][66]

Operators

Main article: List of Mitsubishi A6M Zero operators
 Japan
  • Imperial Japanese Navy Air Service
 Thailand
  • Royal Thai Air Force
  • Royal Thai Navy

Post-war

 Indonesia
  • Indonesian Air Force
 Republic of China
  • Republic of China Air Force

Survivors


A6M2 Model 21 on display at the Pacific Aviation Museum, Pearl Harbor, Hawaii. This aircraft was made airworthy in the early 1980s before it was grounded in 2002.[67]

A6M5 on display at the National Air and Space Museum
Several Zero fighters survived the war and are on display:
  • Japan:
    • Tokyo (Yasukuni War Museum)
    • Hamamatsu (Hamamatsu Air Base)
    • Komaki, Aichi (Mitsubishi Heavy Industries)
    • Iwakuni (MCAS Iwakuni)
    • Kure (Yamato Museum)
    • Kanoya
  • China: Beijing Military Museum
  • The United States:
    • National Air and Space Museum,
    • National Museum of the United States Air Force
    • National Museum of Naval Aviation
    • Pacific Aviation Museum
    • San Diego Air and Space Museum
    • Flying Heritage Collection
    • Planes of Fame Air Museum
  • The UK: Duxford Imperial War Museum - partial airframe
  • New Zealand: Auckland War Memorial Museum
  • Australia: Australian War Memorial in Canberra. A restored A6M2-21 "V-173" was retrieved as a wreck after the war and later found to have been flown by Saburō Sakai at Lae.
  • Indonesia: The Museum Dirgantara Mandala in Yogyakarta has an A6M in its collection.
Another aircraft recovered by the Australian War Memorial Museum in the early 1970s now belongs to Fantasy of Flight in Polk City, Florida. Along with several other Zeros, it was found near Rabaul in the South Pacific. The markings suggest that it was in service after June 1943 and further investigation suggests that it has cockpit features associated with the Nakajima-built Model 52b. If this is correct, it is most likely one of the 123 aircraft lost by the Japanese during the assault of Rabaul. The aircraft was shipped in pieces to the attraction and it was eventually made up for display as a crashed aircraft. Much of the aircraft is usable for patterns and some of its parts can be restored to one day make this a basis for a flyable aircraft.[68]
Four flyable Zero airframes exist. Three have had their engines replaced with similar American units. Only one, the Planes of Fame Museum's A6M5 bearing tail number "61-120" (recovered from Saipan) has the original Sakae engine.[69]
Although not a survivor, the "Blayd" Zero is a reconstruction based on templating original Zero components recovered from the South Pacific. To be considered a "restoration" and not a reproduction, the builders used a small fraction of parts from the original Zero landing gear in the reconstruction.[70][71] Restored as a A6M2 Model 21, it is currently owned by the Texas Flying Legends Museum.[72]
The Commemorative Air Force's A6M3 was recovered from Babo Airfield, New Guinea, in 1991. It was partially restored from several A6M3s in Russia, then brought to the United States for restoration. The aircraft was re-registered in 1998 and displayed at the Museum of Flying in Santa Monica, California. It currently uses a Pratt & Whitney R1830 engine.[73] Another A6M3 was also recovered from Babo Airfield and restored with a P&W engine.[74] It currently is owned by the Flying Heritage Collection in Everett, Washington.[74]
The rarity of flyable Zeros accounts for the use of single-seat North American T-6 Texans, with heavily modified fuselages and painted in Japanese markings, as substitutes for Zeros in the films Tora! Tora! Tora!, The Final Countdown, and many other television and film depictions of the aircraft, such as Baa Baa Black Sheep (renamed Black Sheep Squadron). One Model 52 was used during the production of Pearl Harbor.

Specifications (A6M2 Type 0 Model 21)

Orthographically projected diagram of the Mitsubishi A6M Zero
Data from The Great Book of Fighters[24]
General characteristics
  • Crew: one
  • Length: 9.06 m (29 ft 9 in)
  • Wingspan: 12.0 m (39 ft 4 in)
  • Height: 3.05 m (10 ft 0 in)
  • Wing area: 22.44 m² (241.5 ft²)
  • Empty weight: 1,680 kg (3,704 lb)
  • Loaded weight: 2,410 kg (5,313 lb)
  • Powerplant: 1 × Nakajima Sakae 12 radial engine, 709 kW (950 hp)
  • Aspect ratio: 6.4
Performance
  • Never exceed speed: 660 km/h (356 kn, 410 mph)
  • Maximum speed: 533 km/h (287 kn, 331 mph) at 4,550 m (14,930 ft)
  • Range: 3,105 km (1,675 nmi, 1,929 mi)
  • Service ceiling: 10,000 m (33,000 ft)
  • Rate of climb: 15.7 m/s (3,100 ft/min)
  • Wing loading: 107.4 kg/m² (22.0 lb/ft²)
  • Power/mass: 294 W/kg (0.18 hp/lb)
Armament
  • Guns:

    Divergence of trajectories between 7.7 mm and 20mm ammunition

    • 2× 7.7 mm (0.303 in) Type 97 aircraft machine guns in the engine cowling, with 500 rounds per gun.
    • 2× 20 mm Type 99-1 cannon in the wings, with 60 rounds per gun.
  • Bombs:
    • 2× 60 kg (132 lb) bombs or
    • 1× fixed 250 kg (551 lb) bomb for kamikaze attacks

See also

Related development
  • Nakajima A6M2-N
Aircraft of comparable role, configuration and era
  • Brewster F2A Buffalo
  • Curtiss-Wright CW-21
  • Grumman F4F Wildcat
  • Grumman F6F Hellcat
  • IAR 80
  • Nakajima Ki-43
Related lists

  • List of fighter aircraft
  • List of aircraft of Japan, World War II
  • List of military aircraft of Japan
  • List of aircraft of World War II

Sunday, September 15, 2013

Paper Model Bristol BEAUFIGHTER MK VI F

Bristol BEAUFIGHTER MK VI F Paper Model


Type 156 Beaufighter
The Bristol Beaufighter papercraft model is also the name of a car produced by Bristol Cars in the 1980s.

Type 156 Beaufighter
Beaufighter, armed with rockets
Role Heavy fighter / strike aircraft
Manufacturer Bristol Aeroplane Company
First flight 17 July 1939
Introduction 27 July 1940
Retired 1960 (Australia)
Primary users Royal Air Force
Royal Australian Air Force
Produced May 1940 – 1946
Number built 5,928
Developed from Bristol Beaufort



The Bristol Type 156 Beaufighter, often referred to as simply the Beau, was a British long-range heavy fighter modification of the Bristol Aeroplane Company's earlier Beaufort torpedo bomber design. The name Beaufighter is a portmanteau of "Beaufort" and "fighter".

Unlike the Beaufort, the Beaufighter had a long career and served in almost all theatres of war in the Second World War, first as a night fighter, then as a fighter bomber and eventually replacing the Beaufort as a torpedo bomber. A unique variant was built in Australia by the Department of Aircraft Production (DAP) and was known in Australia as the DAP Beaufighter. paper model


Design and development papercraft model

The idea of a fighter development of the Beaufort was suggested to the Air Ministry by Bristol. The suggestion coincided with the delays in the development and production of the Westland Whirlwind cannon-armed twin-engined fighter. By converting an existing design the "Beaufort Cannon Fighter" could be expected to be developed and produced far quicker than starting a completely fresh design. Accordingly the Air Ministry produced specification F.11/37 written around Bristol's suggestion for an "interim" aircraft pending proper introduction of the Whirlwind. Bristol started building a prototype by taking a part-built Beaufort out of the production line. The prototype first flew on 17 July 1939, a little more than eight months after the design had started and possible due to the use of much of the Beaufort's design and parts. A production contract for 300 machines had already been placed two weeks before the prototype flew, as F.17/39.

In general the differences between the Beaufort and Beaufighter were minor. The wings, control surfaces, retractable landing gear and aft section of the fuselage were identical to those of the Beaufort, while the wing centre section was similar apart from certain fittings. The bomb-bay was omitted, and four forward-firing Hispano 20 mm cannons were mounted in the lower fuselage area. These were initially fed from 60-round drums, requiring the radar operator to change the ammunition drums manually — an arduous and unpopular task, especially at night and while chasing a bomber. As a result, they were soon replaced by a belt-feed system. The cannons were supplemented by six 0.303 inch (7.7 mm) Browning guns in the wings; four in the starboard wing and two to port. The areas for the rear gunner and bomb-aimer were removed, leaving only the pilot in a fighter-type cockpit. The navigator / radar operator sat to the rear under a small perspex bubble where the Beaufort's dorsal turret had been located.

The Bristol Taurus engines of the Beaufort were not powerful enough for a fighter and were replaced by the more powerful Bristol Hercules. The extra power presented problems with vibration; in the final design they were mounted on longer, more flexible struts, which stuck out from the front of the wings. This moved the centre of gravity (CoG) forward, a bad thing for an aircraft design. It was moved back by shortening the nose, as no space was needed for a bomb aimer in a fighter. This put most of the fuselage behind the wing, and moved the CoG back where it should be. With the engine cowlings and propellers now further forward than the tip of the nose, the Beaufighter had a characteristically stubby appearance.

Production of the Beaufort in Australia, and the highly successful use of British-made Beaufighters by the Royal Australian Air Force, led to Beaufighters being built by the Australian Department of Aircraft Production (DAP), from 1944 onwards. The DAP's variant was an attack/torpedo bomber, known as the Mark 21: design changes included Hercules CVII engines, dihedral to the tailplane and enhanced armament.

By the time British production lines shut down in September 1945, 5,564 Beaufighters had been built in England, by Bristol and also by Fairey Aviation Company, (498) Ministry of Aircraft Production (3336) and Rootes (260).
When Australian production ceased in 1946, 365 Mk.21s had been built.

Operational service
Bristol Beaufighter Mk 1 in No. 252 Squadron, North Africa

By fighter standards, the Beaufighter Mk.I was rather heavy and slow. It had an all-up weight of 16,000 lb (7,000 kg) and a maximum speed of only 335 mph (540 km/h) at 16,800 ft (5,000 m). Nevertheless this was all that was available at the time, as the otherwise excellent Westland Whirlwind had already been cancelled due to production problems with its Rolls-Royce Peregrine engines.

The Beaufighter found itself coming off the production line at almost exactly the same time as the first British Airborne Intercept (AI) radar sets. With the four 20 mm cannons mounted in the lower fuselage, the nose could accommodate the radar antennas, and the general roominess of the fuselage enabled the AI equipment to be fitted easily. Even loaded to 20,000 lb (9 t) the plane was fast enough to catch German bombers. By early 1941 it was an effective counter to Luftwaffe night raids. The various early models of the Beaufighter soon commenced service overseas, where its ruggedness and reliability soon made the aircraft popular with crews.

A night-fighter Mk VIF was supplied to squadrons in March 1942, equipped with AI Mark VIII radar. As the faster de Havilland Mosquito took over in the night fighter role in mid to late 1942, the heavier Beaufighters made valuable contributions in other areas such as anti-shipping, ground attack and long-range interdiction in every major theatre of operations.

In the Mediterranean, the USAAF's 414th, 415th, 416th and 417th Night Fighter Squadrons received 100 Beaufighters in the summer of 1943, achieving their first victory in July 1943. Through the summer the squadrons conducted both daytime convoy escort and ground-attack operations, but primarily flew defensive interception missions at night. Although the Northrop P-61 Black Widow fighter began to arrive in December 1944, USAAF Beaufighters continued to fly night operations in Italy and France until late in the war.

By the autumn of 1943 the Mosquito was available in enough numbers to replace the Beaufighter as the primary night fighter of the RAF. By the end of the war some 70 pilots serving with RAF units had become aces while flying Beaufighters.

Coastal Command

1941 saw the development of the Beaufighter Mk.IC long-range heavy fighter. This new variant entered service in May 1941 with a detachment from No. 252 Squadron operating from Malta. The aircraft proved so effective in the Mediterranean against shipping, aircraft and ground targets that Coastal Command became the major user of the Beaufighter, replacing the now obsolete Beaufort and Blenheim.

Coastal Command began to take delivery of the up-rated Mk.VIC in mid 1942. By the end of 1942 Mk VICs were being equipped with torpedo-carrying gear, enabling them to carry the British 18-inch or the US 22.5-inch torpedo externally. The first successful torpedo attacks by Beaufighters came in April 1943, with No. 254 Squadron sinking two merchant ships off Norway.

The Hercules Mk XVII, developing 1,735 hp at 500 feet, was installed in the Mk VIC airframe to produce the TF Mk.X (Torpedo Fighter), commonly known as the "Torbeau." The Mk X became the main production mark of the Beaufighter. The strike variant of the "Torbeau" was designated the Mk.XIC. Beaufighter TF Xs would make precision attacks on shipping at wave-top height with torpedoes or RP-3 rockets. Early models of the Mk Xs carried metric-wavelength ASV (air-to-surface vessel) radar with "herringbone" antennae carried on the nose and outer wings, but this was replaced in late 1943 by the centimetric AI Mark VIII radar housed in a "thimble-nose" radome, enabling all-weather and night attacks.

The North Coates Strike Wing (Coastal Command), based at RAF North Coates on the Lincolnshire coast, developed attack tactics combining large formations of Beaufighters on anti-flak suppression with cannon and rockets while the Torbeaus attacked on low level. These tactics were put into practice in mid 1943 and in a 10-month period 27,000 tonnes of shipping were sunk. Tactics were further adapted when shipping was moved from port during the night. North Coates Strike Wing operated as the largest anti-shipping force of the Second World War, and accounted for over 150,000 tons of shipping and 117 vessels for a loss of 120 Beaufighters and 241 aircrew killed or missing. This was half the total tonnage sunk by all strike wings between 1942-45.
Pacific war
Beaufighter of No. 30 Squadron RAAF over the Owen Stanley Range, New Guinea, 1942.(AWM OG0001)

The Beaufighter arrived at squadrons in Asia and the Pacific in mid-1942. It has often been said — although it was most probably a propaganda invention — that Japanese soldiers referred to the Beaufighter as "whispering death", supposedly because attacking aircraft often were not heard (or seen) until too late. (The Beaufighter's Hercules engines featured sleeve valves which lacked the noisy valve gear common to poppet valve engines. This was most apparent in a reduced noise level at the front of the engine.)

South east Asia

In the South-East Asian Theatre the Beaufighter Mk VIF operated from India on night missions against Japanese lines of communication in Burma and Thailand. The high-speed, low-level attacks were highly effective, despite often atrocious weather conditions, and makeshift repair and maintenance facilities.

South west Pacific

Before DAP Beaufighters arrived at Royal Australian Air Force units in the South West Pacific theatre, the Bristol Beaufighter Mk IC was employed in anti-shipping missions.

The most famous of these was the Battle of the Bismarck Sea in which they co-operated with USAAF A-20 Bostons and B-25 Mitchells. No. 30 Squadron RAAF Beaufighters flew in at mast height to provide heavy suppressive fire for the waves of attacking bombers. The Japanese convoy, under the impression that they were under torpedo attack, made the fatal tactical error of turning their ships towards the Beaufighters, leaving them exposed to skip bombing attacks by the US medium bombers. The Beaufighters inflicted maximum damage on the ships' anti-aircraft guns, bridges and crews during strafing runs with their four 20 mm (0.787 in) nose cannons and six wing-mounted .303 in (7.7 mm) machine guns. Eight transports and four destroyers were sunk for the loss of five aircraft, including one Beaufighter.
Postwar

From late 1944, RAF Beaufighter units were engaged in the Greek Civil War, finally withdrawing in 1946.

The Beaufighter was also used by the air forces of Portugal, Turkey and the Dominican Republic. It was used briefly by the Israeli Air Force.

Variants

Beaufighter Mk IF
Two-seat night fighter variant.

Beaufighter Mk IC
The "C" stood for Coastal Command variant; many were modified to carry bombs.

Beaufighter Mk II
However well the Beaufighter performed, the Short Stirling bomber program by late 1941 had a higher priority for the Hercules engine and the Rolls Royce Merlin XX-powered Mk II was the result.

Beaufighter Mk IIF
Production night fighter variant.
Beaufighter Mk III/IV
The Mark III and Mark IV were to be Hercules and Merlin powered Beaufighters with a new slimmer fuselage carrying an armament of 6 cannon and 6 machine guns which would give performance improvements. The necessary costs of making the changes to the production line led to the curtailing of the Marks. [1]

Beaufighter Mk V
The Vs had a Boulton Paul turret with four 0.303 machine guns mounted aft of the cockpit supplanting one pair of cannons and the wing-mounted machine guns. Only two Mk Vs were built.

Beaufighter Mk VI
The Hercules returned with the next major version in 1942, the Mk VI, which was eventually built to over 1,000 examples.

Beaufighter Mk VIC
Torpedo-carrying variant dubbed the "Torbeau".

Beaufighter Mk VIF
This variant was equipped with AI Mark VIII radar.

Beaufighter Mk VI (ITF)
Interim torpedo fighter version.

Beaufighter TF Mk X
Two-seat torpedo fighter aircraft. The last major version (2,231 built) was the Mk X, among the finest torpedo and strike aircraft of its day.

Beaufighter Mk XIC
Built without torpedo gear for Coastal Command use.

Beaufighter Mk 21
The Australian-made DAP Beaufighter. Changes included Hercules CVII engines, a dihedral tailplane, four 20 mm in the nose, four Browning .50 in the wings and the capacity to carry eight five-inch High-Velocity Aircraft Rockets (HVAR), two 250 lb bombs, two 500 lb bombs and one Mk13 torpedo.

Beaufighter TT Mk 10
After the war, many RAF Beaufighters were converted into target tug aircraft.






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