The Japanese Navy Mitsubishi A6M Zero carrier-borne fighter became synonymous with the Japanese military commitment over Asia and the Pacific during World War 2.
The Mitsubishi A6M "Rei-sen" was the primary naval fighter of the Japanese Empire heading into World War 2. The aircraft was recognized by its pilots as the "Zero-sen" based on the Imperial Year calendar (1940 at the time). The Allies eventually adopted the "Zero" name as the type's nickname while the official Allied codename for the became "Zeke". The A6M received much attention in the early stages of the war in the Pacific where it became the first naval aircraft to be able to best any of its land-based counterparts through a combination of speed, maneuverability and range. Mitsubishi Heavy Industries of Japan produced some 10,939 examples from 1940 on. The series survived the whole of the war up to the Japanese surrender of September 1945, its worth having been proven over five years of conflict.
Origins of the A6M lay in pre-war 1937 by which time Mitsubishi had just delivered the A5M. The A5M was a monoplane fighter developed for the Imperial Japanese Navy and incorporated a streamlined fuselage, low, forward-set monoplane wings and a single-seat cockpit. While 1,094 of the type were taken into inventory, the type still held some old-fashioned design elements which rendered it an obsolete-appearing aircraft by World War 2 standards. It held an open-air cockpit for the pilot with a raised fuselage spine and fixed, spatted main landing gear legs. Visibility out of the cockpit was poor and armament centered on a pair of 7.7mm Type 89 series machine guns.
With these limitations in mine, the Imperial Japanese Navy pushed both Mitsubishi and Nakajima for a new carrier-borne naval fighter of greater capability - particularly range to prove important over the vast spans of Pacific Ocean in the upcoming Japanese campaign. Also, the hitting power of the aircraft was to be improved by implementation of cannon armament coupled to machine guns for a formidable one-two punch. Due to the space on Japanese carriers, the aircraft would also have to be relatively compact and feature folding wing assemblies for storage. The IJN sought particular specifications out of their new mount: a maximum speed of 310 miles per hour and a climb rate of 9,850 feet reached in 3.5 minutes.
The initial prototype was unveiled on March 16th, 1939 and achieved first flight on April 1st of that year. On September 14th, the aircraft was officially adopted by the IJN as its new standardized carrier-based fighter mount. Initial aircraft were powered by a Mitsubishi engine (Zuisei line) until a decided shift was made towards a Nakajima product. The Mitsubishi aircraft was adopted as the A6M "Zero-sen" Type 00 Fighter and saw its first service in July of 1940 against the Chinese. It quickly proved itself the finest fighter in the world and bested nearly all opponents in the Asian and Pacific theaters and certainly alerted observers in Washington, D.C. and elsewhere but nothing was done to further investigate the type.
Production of A6Ms eventually eclipsed all other Japanese aircraft of the war. Mitsubishi was its maker but additional manufacture was handled through competitor Nakajima who produced over 6,200 examples alone. Additional production was seen from Hitachi and Sasebo and included a floatplane derivative which also saw extensive service in the war.
By the time of the Japanese surprise attack on Pearl Harbor, Hawaii, on December 7th, 1941, the IJN managed a stable of some 400 Zero fighters and the carrier groups to field them. Zeros took part in the devastating attacks which rendered many USN warships useless or damaged and thrust the United States into a formal war declaration against the Empire of Japan. From there on, the A6M was fielded in all major Japanese campaigns and retained its air dominance heading into 1942 and 2 x 132lb bombs were added for the ground strike role. The aircraft now deserved the respect of Washington observers and its capabilities were fully noticed.
It was not until the middle of 1942 that the Allies managed to capture an intact A6M and study it from the inside out back in the United States. It was from this work that the weaknesses of the Mitsubishi aircraft were soon discovered and new counter tactics arranged for Allied pilots. The lack of armoring proved a critical design flaw in the Zero and Allied pilots would work at exploiting this fatal flaw. Additionally, the United States Navy was now turning to more modern, capable fighting mounts in their F6F Hellcats and F4U Corsairs replacing outgoing frontline types like the F4F Wildcats. The turning point in the early stages of the Pacific war then came at the Battle of Midway in June of 1942 where these new American fighters squared off against incoming waves of Zeros and earned a tremendous victory in the process. The Americans benefitted from armoring of critical components, improved weaponry and tactics and increased performance from dominant engines. Against this, the Zero had now met its official match.
From 1943 onwards, the Zero proved a far lesser, more vulnerable foe than seen in the early stages of the war. A "definitive" Zero was produced as the A6M8 which incorporated a Nakajima Kinsei engine of 1,560 horsepower but the arrival of this variant proved a moot addition. Tide had shifted away from the Japanese Empire and for the Allies and territorial losses mounted into 1945. The Zero was eventually relegated as a carrier for suicidal airmen in the kamikaze strikes that followed. These were outfitted with 1 x 550lb bombs for maximum carnage.
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(OPERATORS list includes past, present, and future operators when applicable)
✓Air-to-Air Combat, Fighter
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
✓Maritime / Navy
Land-based or shipborne capability for operating over-water in various maritime-related roles while supported by allied naval surface elements.
SYNCHRONIZED / INTERRUPTOR GEAR
Automatic weapons are synchronized to fire through the spinning propeller blades via special mechanical gear arrangement.
FOLDING WING(S)
Mainplanes are designed to fold, improving storage on land and at sea.
HIGH-SPEED PERFORMANCE
Can accelerate to higher speeds than average aircraft of its time.
HIGH-ALTITUDE PERFORMANCE
Can reach and operate at higher altitudes than average aircraft of its time.
EXTENDED RANGE PERFORMANCE
Capability to travel considerable distances through onboard fuel stores.
SUPER PERFORMANCE
Design covers the three all-important performance categories of speed, altitude, and range.
MARITIME OPERATION
Ability to operate over ocean in addition to surviving the special rigors of the maritime environment.
BAILOUT PROCESS
Manual process of allowing its pilot and / or crew to exit in the event of an airborne emergency.
ENCLOSED CREWSPACE(S)
Features partially- or wholly-enclosed crew workspaces.
RETRACTABLE UNDERCARRIAGE
Features retracting / retractable undercarriage to preserve aerodynamic efficiency.
Length
29.7 ft (9.06 m)
Width/Span
36.1 ft (11.00 m)
Height
9.8 ft (2.98 m)
Empty Wgt
4,136 lb (1,876 kg)
MTOW
6,025 lb (2,733 kg)
Wgt Diff
+1,889 lb (+857 kg)
(Showcased structural values pertain to the Mitsubishi A6M5 Rei-sen (Zero) production variant)
monoplane / low-mounted / straight
Monoplane
Design utilizes a single primary wing mainplane; this represent the most popular mainplane arrangement.
Low-Mounted
Mainplanes are low-mounted along the sides of the fuselage.
Straight
The planform involves use of basic, straight mainplane members.
(Structural descriptors pertain to the Mitsubishi A6M5 Rei-sen (Zero) production variant)
Installed:
1 x Nakajima NK1C Sakae 21 14-cylinder, two-row, air-cooled radial piston engine developing 1,130 horsepower driving three-bladed propeller unit at the nose.
(Showcased performance specifications pertain to the Mitsubishi A6M5 Rei-sen (Zero) production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
STANDARD:
2 x 20mm Type 99-1 automatic cannons in wings (one gun to a wing member).
2 x 7.7mm Type 97 machine guns in engine cowling synchronized to fire through the spinning propeller blades.
OPTIONAL:
2 x 130lb conventional drop bombs.
1 x 550lb bomb (for kamikaze role).
Supported Types
(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 3
Mounting Points
-
-
-
-
5
-
1
-
4
-
-
-
-
HARDPOINT(S) KEY:
X
15
13
11
9
7
5
3
1
2
4
6
8
10
12
14
COLOR KEY:
Fuselage Centerline
Fuselage Port/Wingroot
Fuselage Starboard/Wingroot
Wing/Underwing
Wingtip Mount(s)
Internal Bay(s)
Not Used
Note: Diagram above does not take into account inline hardpoints (mounting positions seated one-behind-the-other).
A6M1 - Prototype Model Designation fitted with 780hp Mitsubishi Zuisei 13 radial piston engine.
A6M2 - Initial Production Model Designation fitted with 950hp Nakajima Sakae 12 radial piston engine.
A6M2-N - Naval Float Version dubbed "Rufe" by Allied forces.
A6M3 - Fitted with two-stage supercharged Sakae engine; sans folding wingtips.
A6M5 - Fitted with Sakae 21 radial piston engine; improved exhaust system; multiple subvariants of this model existed.
A6M6 - Fitted with water-methanol boosted Sakae 31 engine.
A6M7 - Fighter / Dive-Bomber Hybrid.
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
Overall Rating
The overall rating takes into account over 60 individual factors related to this aircraft entry.
84
Rating is out of a possible 100 points.
Relative Maximum Speed
Hi: 400mph
Lo: 200mph
This entry's maximum listed speed (354mph).
Graph average of 300 miles-per-hour.
City-to-City Ranges
NYC
LON
LON
PAR
PAR
BER
BER
MOS
MOS
TOK
TOK
SYD
SYD
LAX
LAX
NYC
Mitsubishi A6M5 Rei-sen (Zero) operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
Design Balance
The three qualities reflected above are altitude, speed, and range.
Aviation Era Span
Showcasing era cross-over of this aircraft design.
Unit Production (10,938)
10938
36183
44000
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).
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Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.
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China; Imperial Japan; Indonesia; Taiwan; Thailand
