A6M1, Type 0 Prototypes In March 1939, the first two A6M1 prototypes were completed, powered by the
Mitsubishi Zuisei 13 engine with a two-blade propeller. It first flew on 1 April, and passed testing within a remarkably short period. 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.
A6M2a Type 0 Model 11 While the Navy was testing the first two prototypes, they suggested that the third be fitted with the
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
Chongqing 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 when 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 slowly filtered back to the US. They were met with scepticism by most US military officials, who thought it impossible for the Japanese to build such an aircraft.
A6M2b Type 0 Model 21 '' prior to attack on Pearl Harbor, 7 December 1941 After the delivery of the 65th aircraft, a further change was worked into the production lines, which introduced folding wingtips to allow them to fit on aircraft carriers.
A6M3 Type 0 Model 32 In 1941, Nakajima introduced the Sakae 21 engine, which used a two-speed
supercharger for better altitude performance, and increased power to . A prototype Zero with the new engine was first flown on 15 July 1941. 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 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 to . 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. 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 . The two 20 mm wing cannon were upgraded from the
Type 99 Mark 1 to the Mark 2, Consequently, the Model 32 was unsuited to that campaign and was used mainly for shorter range offensive missions and interception. This variant was flown by only a small number of units, and only 343 were built. One example survives today, and is on display at the
Tachiarai Peace Memorial Museum in
Tachiarai, Fukuoka.
A6M3 Type 0 Model 22 In order to correct the deficiencies of the Model 32, a new version with folding wingtips and redesigned wing was introduced. The fuel tanks were moved to the outer wings, fuel lines for a drop tank were installed under each wing and the internal fuel capacity was increased to . More importantly, it regained its capabilities for long operating ranges, similar to the previous A6M2 Model 21, which was vastly shortened by the Model 32. Before the new design type was accepted formally by the Navy, the A6M3 Model 22 already stood ready for service in December 1942. Approximately 560 aircraft of the new type had been produced in the meantime by Mitsubishi Jukogyo K.K. According to a theory, the very late production Model 22 might have had wings similar to the shortened, rounded-tip wing of the Model 52. One plane of such arrangement was photographed at
Lakunai Airfield ("Rabaul East") in the second half of 1943, and has been published widely in a number of Japanese books. While the engine cowling is the same as on the previous Models 32 and 22, the theory proposes that the plane is an early-production Model 52. The Model 32, 22, 22 Kō, 52, 52 Kō and 52 Otsu were all powered by the Nakajima Sakae Mod. 21 engine. Mitsubishi's involvement in the project was probably quite limited or nonexistent; the unmodified Sakae engine was made by Nakajima. 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 it did not bestow model numbers 41 or 42 formally, although it appears that the arsenal did use the designation "A6M4". Despite these failures, the prototype engines nevertheless provided useful experience for future engine designs.
A6M5 Type 0 Model 52 , captured by US forces. Sometimes considered to be the most effective variant, 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. Produced first by Mitsubishi, most Model 52s were made by Nakajima. In June 1943, the prototype was made by modifying an A6M3 and was first flown in August 1943. The first Model 52 is said in the handling manual to have production number 3904, which apparently refers to the prototype. Research by Mr. Bunzo Komine published by Mr. Kenji Miyazaki states that the aircraft 3904 to 4103 had the same exhaust system and cowl flaps as on the Model 22. This is partially corroborated by two wrecks researched by Mr. Stan Gajda and Mr. L. G. Halls, with production numbers 4007 and 4043, respectively. The upper cowling was slightly redesigned from that of the Model 22. From number 4354, the radio became the Model 3, aerial Mark 1, at which point the antenna mast was shortened slightly. To production number 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. Nakajima manufactured the Model 52 at its Koizumi plant in
Gunma Prefecture. The A6M5 had a maximum speed of at , reaching that altitude in 7 minutes and 1 second. Subsequent variants included: • A6M5a, Model (
Kō, 52a) – Starting at Mitsubishi number 4651, an armament change substituted the belt-fed Type 99-2 Mark 4 cannon, with 125 rounds per gun, in place of the drum-fed Type 99-2 Mark 3 cannon that carried 100 rounds per gun. Hence, the bulge in the underside of the wing for each cannon's ammunition drum was deleted and the ejection port for spent cartridge cases was moved. Thicker wing skinning was installed to permit higher diving speeds. • A6M5b, Model (
Otsu, 52b) – Armament change: The 7.7 mm (.303 in) Type 97 gun ( muzzle velocity and range) in the right forward fuselage was replaced by a 13.2 mm
Type 3 Browning-derived gun ( muzzle velocity and range, with a rate of fire of 800 rounds per minute) 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. Each wing cannon received a fairing at the wing leading edge. A plate of armored glass thick was fitted to the windscreen. A larger propeller spinner was fitted, suggesting a change to the propeller. The type of ventral drop tank was changed, it now had fins and was suspended on a slanted pipe. The first of this variant was completed in April 1944 and it was produced until October 1944. • A6M5c, Model (
Hei, 52c) – Armament change: One 13.2 mm (.51 in) Type 3 machine gun was added in each wing outboard of the cannon, and the 7.7 mm gun on 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 A thick piece of armored glass was installed at the headrest and an thick plate of armor was installed behind the seat. The mounting of the central drop tank changed to a four-post design. Wing skin was thickened further. The first of this variant was completed in September 1944. • 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. They were armed with one 20 mm Type 99 cannon behind the pilot, aimed upward, similar in intent to the Luftwaffe's
Schräge Musik installation. A lack of radar prevented them from being very effective. Some Model 21 and 52 aircraft were converted to "bakusen" (
fighter-bombers) by mounting a bomb rack and bomb in place of the centerline drop tank. Up to seven Model 52 planes were ostensibly converted into A6M5-K two-seat trainers.
A6M6 Type 0 Model 53 The A6M6 was developed to use the Sakae 31a engine, featuring water-methanol engine boost and self-sealing wing tanks. During preliminary testing, its performance was considered unsatisfactory due to the additional engine power failing to materialize and the unreliability of the fuel injection system. Testing continued on the A6M6 but the end of war stopped further development. Only one prototype was produced.
A6M7 Type 0 Model 62/63 The A6M7 was the last variant to see service. It was designed to meet a requirement by the Navy for a dedicated
attack/
dive bomber version that could operate from smaller aircraft carriers The A6M7 had considerable design changes compared to previous attempts to make the A6M suitable for dive bombing. This included a reinforced vertical stabilizer, a special bomb rack, provision of two drop tanks and fixed bomb/rocket swing stoppers on the underside of the wings.
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 , 60% more powerful than the A6M2's engine. The Model 64 was modified to carry two drop tanks on either wing in order to permit the mounting of a 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 A6M8s, only the two prototypes being completed and flown. ==Production==