Equipment, armament and combat composition of the Japanese Air Force: history and modernity. Below, according to the foreign press, are the organization and composition, combat training and development prospects of the Japanese Air Force Japanese military aircraft

Since the end of World War II, the Japanese military-industrial complex has not shined with the “pearls” of its military industry, and has become completely dependent on the imposed products of the American defense industry, the powerful lobby of which was carried out by the Japanese authorities due to the direct dependence of capital and pro-American sentiments in the mentality of the top of society .

A striking example of this is the modern composition of the Air Force (or Air Self-Defense Forces): these are 153 F-15J units (a complete copy of the F-15C), 45 F-15DJ units (a copy of the two-seater F-15D). At the moment, it is these machines, built under an American license, that form the quantitative backbone of aviation for gaining air superiority, as well as suppressing air defense;

The rest of the fighter-reconnaissance aviation copied from the United States is represented by the F-4EJ, RF-4EJ, EF-4EJ aircraft, of which there are about 80 in the country's Air Force, now they are gradually being withdrawn from service. There is also a contract for the purchase of 42 F-35A GDP fighters, which are an improved copy of the Yak-141. RTR aviation, like the leaders in Europe, is represented by E-2C and E-767 aircraft.

December 18, 2012 Japanese F-2A escorts the latest Russian naval reconnaissance aircraft Tu-214R

But in 1995, the Japanese military pilot E. Watanabe took to the air a completely new combat vehicle, which can now be safely classified as a 4 ++ generation. It was the first prototype of the XF-2A multi-role fighter F-2A, and the subsequent two-seat F-2B. Despite the strong similarity of the F-2A with the American F-16C Block 40, namely, it was taken by Japanese engineers as a reference model, the F-2A was a relatively new technical unit.

Most of all, this affected the airframe and avionics. The nose of the fuselage is a purely Japanese development using a new geometric idea that is different from the Falcon.

It boasts the F-2A and a completely new wing with a lower sweep, but 1.25 greater aerodynamic lifting coefficient (carrying property): the wing area of ​​the Falcon is 27.87 m 2, the F-2 has 34.84 m 2 . Thanks to the increased wing area, the Japanese embodied in their fighter the ability to "energy" maneuver in the BVB in the steady turn mode at a speed of about 22.5 deg / s, as well as reduce fuel consumption during high-altitude combat duty in the complex island grid of Japan. It also became possible thanks to the use of advanced composite materials in the airframe elements of the new aircraft.



The increase in maneuverability was also influenced by the large area of ​​the elevators.

The engine nacelle remained standard for the Falcon, since it was decided to use the General Electric F110-GE-129 turbojet afterburner engine with a maximum thrust of 13.2 tons. PTB. The latest American F-16C Block 60 has only 3080 liters in internal tanks. The Japanese made a very wise move: referring to their defensive nature of the aircraft, in cases of conflict, within Japan only, they made it possible for the F-2A to have more fuel on board, and maintain maneuverability at a high level, without using massive PTBs. Due to this, a higher combat radius of action, which is about 830 km against 580 for the Falcon.

The fighter has a practical ceiling of more than 10 km, flight speed at high altitude is about 2120 km/h. When installing 4xUR AIM-9M (4x75kg) and 2xUR AIM-120C (2x150kg) and 80% filled internal fuel tanks (3040l), the thrust-to-weight ratio will be about 1.1, which even today is a strong indicator.

The avionics, at the time the fighter entered the Air Force, gave odds to the entire Chinese fleet. The aircraft is equipped with a Mitsubishi Electric multi-channel noise-immune radar with J-APG-1 AFAR, the antenna array of which is formed by 800 PPM made of GaAs (gallium arsenide), which is the most important semiconductor compound used in modern radio engineering.

The radar is capable of carrying out a "tie" (SNP) of at least 10 target routes, and firing 4-6 of them. Considering that in the 1990s the PAR industry was actively developing in the Russian Federation and other countries, it can be judged that the radar operating range for a fighter-type target (3 m 2) is no more than 120-150 km. However, at that time, AFAR and PFAR were only on the French Rafale, our MiG-31B and the American F-22A.

Airborne radar J-APG-1

The F-2A is equipped with a Japanese-American digital autopilot, a Melko electronic warfare system, communication and tactical situation data transmission devices in the short and ultrashort wave bands. The inertial navigation system is built around five gyroscopes (the main one is laser, and four backup mechanical ones). The cockpit is equipped with a high-quality holographic indicator on the windshield, a large tactical information MFI, and two monochrome CRT MFIs.

The armament is almost identical to the American F-16C, and is represented by AIM-7M, AIM-120C, AIM-9L,M,X; It is worth noting the prospect of the Japanese AAM-4 air-to-air missile system, which will have a range of about 120 km and a flight speed of 4700-5250 km / h. It will be able to use a fighter and guided bombs with PALGSN, ASM-2 anti-ship missiles and other advanced weapons.

Now the Japan Air Self-Defense Force has 61 F-2A and 14 F-2B fighters, which, along with AWACS and 198 F-15C fighters, provide good air defense for the country.

In the 5th generation of fighter aviation, Japan is already “walking” on its own, which is confirmed by the Mitsubishi ATD-X “Shinshin” project (“Shinshin”, which means “soul”).

Japan, like every technological superpower, by definition must have its own stealth fighter to gain air supremacy; the beginning of work on the magnificent descendant of the legendary A6M Zero aircraft started back in 2004. It can be said that the employees of the Technical Design Institute of the Ministry of Defense approached the stages of creating the nodes of a new machine in a “different plane”.

Since the Xingxing project received its first prototype much later than the F-22A, and, undoubtedly, all the shortcomings and errors that the Russians, Americans and Chinese learned from were taken into account and eliminated, and all the best aerodynamic ideas for implementation of ideal performance characteristics, the latest developments in the avionics database, where Japan has already succeeded.

The first flight of the prototype ATD-X is scheduled for the winter of 2014-2015. Only for the development of the program and the construction of an experimental machine in 2009, an allocation of 400 million dollars was allocated. Most likely, the Xingsin will be called the F-3, it will enter the troops no earlier than 2025.

Shinshin is the smallest fifth-generation fighter, yet the expected range is about 1800 km

What do we know about Xingsin today? Japan is a small power, and does not plan to independently participate in major regional wars with the Self-Defense Air Force, sending its combat aircraft thousands of kilometers deep into enemy territories, hence the name of the Self-Defense Armed Forces. Therefore, the dimensions of the new "invisible" are small: length - 14.2 m, wingspan - 9.1 m, height along the rear stabilizers - 4.5 m. There is room for one crew member.

Based on the small size of the airframe and the widest use of composite materials, and this is more than 30% plastic with reinforcing carbon, 2 lightweight XF5-1 turbofan engines with a thrust of about 5500 kg / s each, the mass of an empty fighter will be in the range of 6.5-7 tons, t .e. weight and overall dimensions will be very close to the French fighter Mirage-2000-5.

Due to the miniature midsection and the maximum slope of the air intakes to the longitudinal axis of the aircraft (better than that), as well as the minimum number of right angles in the design of a sophisticated airframe, the Shinsina EPR should meet the expectations of the Japanese military flight crew, and not exceed 0.03 m 2 ( F-22A has about 0.1 m 2, T-50 has about 0.25 m 2). Although, according to the developers, the equivalent of a “small bird” sounded, and this is 0.007 m 2.

Shinsina engines are equipped with an all-aspect OVT system, consisting of three controlled aerodynamic petals that look very “oak”, like for a 5+ generation fighter, but apparently Japanese engineers saw in this design some guarantees of greater reliability than our “all-aspect” on the product 117C. But in any case, this nozzle is better than the American one, set to , where the vector control is performed only in pitch.

The avionics architecture is planned to be built around the powerful J-APG-2 airborne radar with AFAR, the detection range of the F-16C type target will be about 180 km, close to the Zhuk-A and AN / APG-80 radars, and a multi-channel data bus based on fiber-optic conductors, controlled by the most powerful on-board computers. In the context of the progress of Japanese electronics, this can be seen firsthand.

The armament will be very diverse, with placement in the internal compartments of the fighter. With OVT, the aircraft partially realizes super-maneuverable qualities, but due to the smaller ratio of the wingspan to the length of the fuselage than other aircraft (Xinsin has 0.62, PAK-FA has 0.75), a glider with an aerodynamic bearing structure, as well as developed forward influxes at the wing roots, the absence of a statically unstable scheme in the airframe, there is no possibility of an emergency transition to high-speed unsteady flight. In BVB, this aircraft is more inherent in medium-speed "energy" maneuvering using OVT.

"Three-leaf" OVT on each turbofan engine

Previously, the Land of the Rising Sun wanted to conclude a contract with the United States for the purchase of several dozen Raptors, but the American military leadership, with its unequivocal position of complete non-proliferation in the field of "precise" defense, refused to provide the Japanese side with even a "depleted version" of the F-22A.

Then, when Japan began testing the first ATD-X layout, and asked for a special wide-range electromagnetic StingRay-type test site for all-angle scanning of the EPR indicator, they again “wiped their feet” on their Pacific partner. The French side agreed to provide the installation, and things went further ... Well, let's see how the sixth fifth-generation fighter will surprise us at the end of the year.

/Evgeny Damantsev/

After the defeat of Imperial Japan in World War II, the country under American occupation was prohibited from having its own armed forces. In the Constitution of Japan adopted in 1947, the rejection of the creation of armed forces and the right to wage war was proclaimed. However, in 1952, the National Security Forces were formed, and in 1954, the Japan Self-Defense Forces began to be created on their basis.


Formally, this organization is not the armed forces and in Japan itself is considered a civilian agency. The Prime Minister of Japan is in command of the Self-Defense Forces. Nevertheless, this "non-military organization" with a budget of $59 billion and a staff of almost 250,000 people is equipped with fairly modern equipment.

Simultaneously with the creation of the Self-Defense Forces, the reconstruction of the Air Force - the Japan Air Self-Defense Forces - began. In March 1954, Japan concluded a military assistance treaty with the United States, and in January 1960, a "treaty of mutual cooperation and security guarantees" was signed between Japan and the United States. In accordance with these agreements, the Air Self-Defense Force began to receive American-made aircraft. The first Japanese air wing was organized on 1 October 1956 with 68 T-33As and 20 F-86Fs.


F-86F fighters of the Japan Air Self-Defense Force

In 1957, licensed production of the American F-86F Saber fighters began. Mitsubishi built 300 F-86Fs between 1956 and 1961. These aircraft served in the Air Self-Defense Force until 1982.

After the F-86F was put into service and the licensed production of the F-86F aircraft began, the Air Self-Defense Forces needed two-seat jet training aircraft (TCA), which are close in their characteristics to combat fighters. Produced by Kawasaki Corporation under license, the T-33 jet trainer with a straight wing (210 aircraft built), created on the basis of the first serial American jet fighter F-80 Shooting Star, did not fully meet the requirements.

In this regard, Fuji developed the T-1 TCB based on the American F-86F Saber fighter. Two crew members were placed in the cockpit in tandem under a common, reclining lantern. The first plane took off in 1958. Due to problems with the refinement of the Japanese-designed engine, imported British Bristol Aero Engines Orpheus engines with a thrust of 17.79 kN were installed on the first version of the T-1.


Japanese TCB T-1

The aircraft was recognized as meeting the requirements of the Air Force, after which two batches of 22 aircraft were ordered under the designation T-1A. Aircraft of both batches were delivered to the customer in 1961-1962. From September 1962 to June 1963, 20 production aircraft were built under the designation T-1B with a Japanese Ishikawajima-Harima J3-IHI-3 engine with a thrust of 11.77 kN. Thus, the UTS T-1 became the first post-war Japanese jet aircraft designed by its own designers, the construction of which was carried out at national enterprises from Japanese components.

The Japanese Air Self-Defense Force operated the T-1 trainer for over 40 years, several generations of Japanese pilots were trained on this training aircraft, the last aircraft of this type was decommissioned in 2006.

With a takeoff weight of up to 5 tons, the aircraft reached speeds of up to 930 km/h. It was armed with one machine gun of 12.7 mm caliber, could carry a combat load in the form of NAR or bombs weighing up to 700 kg. In terms of its main characteristics, the Japanese T-1 roughly corresponded to the widespread Soviet UTS - UTI MiG-15.

In 1959, the Japanese company Kawasaki acquired a license to manufacture the Lockheed P-2N Neptune anti-submarine patrol aircraft. Since 1959, mass production began at the plant in the city of Gifu, culminating in the production of 48 aircraft. In 1961, Kawasaki began developing its own modification of the Neptune. The aircraft received the designation P-2J. On it, instead of piston engines, two General Electric T64-IHI-10 turboprop engines with a power of 2850 hp, produced in Japan, were installed. Auxiliary Westinghouse J34 turbojets were replaced with Ishikawajima-Harima IHI-J3 turbojets.

In addition to the installation of turboprop engines, there were other changes: the fuel supply was increased, new anti-submarine and navigation equipment was installed. In order to reduce drag, the engine nacelles were redesigned. To improve take-off and landing characteristics on soft ground, the landing gear was redesigned - instead of one large diameter wheel, the main struts received twin wheels of a smaller diameter.


Kawasaki P-2J maritime patrol aircraft

In August 1969, serial production of the P-2J began. Between 1969 and 1982, 82 cars were produced. Patrol aircraft of this type were operated by Japanese naval aviation until 1996.

Realizing that the American F-86 subsonic jet fighters no longer met modern requirements by the beginning of the 60s, the command of the Self-Defense Forces began to look for a replacement for them. In those years, the concept became widespread, according to which air combat in the future would be reduced to supersonic interception of attack aircraft and missile duels between fighters.

These ideas were fully consistent with the Lockheed F-104 Starfighter supersonic fighter developed in the USA at the end of the 50s.

During the development of this aircraft, high speed performance was put at the forefront. The Starfighter was later often referred to as "a rocket with a man inside". The pilots of the US Air Force quickly became disillusioned with this capricious and emergency aircraft, and they began to offer it to the allies.

"Starfighter" in the late 1950s, despite the high accident rate, became one of the main fighters of the Air Force of many countries, was produced in various modifications, including in Japan. It was an all-weather F-104J interceptor. On March 8, 1962, the first Japanese-assembled Starfighter rolled out of the Mitsubishi plant in Komaki. By design, it almost did not differ from the German F-104G, and the letter "J" denotes only the country of the customer (J - Japan).

Since 1961, the Air Force of the Land of the Rising Sun has received 210 Starfighter aircraft, of which 178 were produced by the Japanese concern Mitsubishi under license.

In 1962, construction began on the first Japanese turboprop airliner for short and medium haul lines. The aircraft was manufactured by the consortium Nihon Aircraft Manufacturing Corporation. It included almost all Japanese aircraft manufacturers, such as Mitsubishi, Kawasaki, Fuji and Shin Meiwa.

The passenger turboprop, designated YS-11, was intended to replace the Douglas DC-3 on domestic flights and could carry up to 60 passengers at a cruising speed of 454 km/h. From 1962 to 1974, 182 aircraft were produced. To date, the YS-11 remains the only commercially successful passenger aircraft produced by a Japanese company. Of the 182 aircraft produced, 82 aircraft were sold to 15 countries. A dozen of these aircraft were delivered to the military department, where they were used as transport and training aircraft. Four aircraft were used in the electronic warfare version. In 2014, a decision was made to write off all variants of the YS-11.

By the mid-1960s, the F-104J was beginning to be regarded as obsolete. Therefore, in January 1969, the Japanese cabinet raised the issue of equipping the country's air force with new fighter-interceptors, which were supposed to replace the Starfighters. The American F-4E "Phantom" third-generation multirole fighter was chosen as the prototype. But the Japanese, when ordering the F-4EJ variant, set the condition that it be a "clean" fighter-interceptor. The Americans did not object, and all equipment for working on ground targets was removed from the F-4EJ, but the air-to-air armament was strengthened. Everything in it was made in line with the Japanese concept of "defense only".

The first licensed Japanese-built aircraft first flew on May 12, 1972. Mitsubishi subsequently built 127 F-4FJs under license.

A "softening" of Tokyo's approaches to offensive types of weapons, including in the Air Force, began to be observed in the second half of the 1970s under pressure from Washington, especially after the adoption in 1978 of the so-called "Guidelines for Japan-US Defense Cooperation." Prior to this, no joint actions, even exercises, of self-defense forces and American units were conducted on the territory of Japan. Since then, much, including in the performance characteristics of aviation equipment, in the Japanese Self-Defense Forces has been changing based on joint offensive operations.

For example, the F-4EJ fighters, which were still being produced, began to install equipment for refueling in the air. The last Phantom for the Japanese Air Force was built in 1981. But already in 1984, a program was adopted to extend their service life. At the same time, the Phantoms began to be equipped with bombing equipment. These aircraft were named Kai. Most of the "Phantoms" that had a large residual resource were upgraded.

F-4EJ Kai fighters continue to be in service with the Japan Air Self-Defense Force. Recently, about 10 aircraft of this type are decommissioned annually. About 50 F-4EJ Kai fighters and RF-4EJ reconnaissance aircraft are still in service. Apparently, machines of this type will be finally decommissioned after receiving the American F-35A fighters.

In the early 60s, the Japanese company Kawanishi, known for its seaplanes, renamed Shin Maywa, began research on the creation of a new generation of anti-submarine seaplanes. In 1966, the design was completed, and in 1967 the first prototype took to the air.

The new Japanese flying boat, designated PS-1, was a cantilever high-wing aircraft with a straight wing and a T-tail. The design of the seaplane is all-metal single-row, with a pressurized semi-monocoque fuselage. The power plant is four T64 turboprop engines with an HP 3060 power. , each of which drove a three-bladed propeller. There are floats under the wing for additional stability during takeoff and landing. A retractable wheeled chassis is used to move along the slipway.

To solve anti-submarine tasks, the PS-1 had a powerful search radar, a magnetometer, a receiver and indicator of sonobuoy signals, a flyover indicator, as well as active and passive submarine detection systems. Under the wing, between the engine nacelles, there were nodes for hanging four anti-submarine torpedoes.

In January 1973, the first aircraft entered service. Following the prototype and two pre-production machines, a batch of 12 serial machines followed, and then eight more aircraft. During the period of operation, six PS-1s were lost.

Subsequently, the Maritime Self-Defense Forces abandoned the use of the PS-1 as an anti-submarine aircraft, and all the vehicles remaining in the ranks were focused on search and rescue missions at sea, anti-submarine equipment from seaplanes was dismantled.


Seaplane US-1A

In 1976, the US-1A search and rescue version appeared with higher power T64-IHI-10J engines of 3490 hp each. Orders for the new US-1A were received in 1992-1995, in total, 16 aircraft were ordered by 1997.
There are currently two US-1A search and rescue aircraft in Japanese Naval Aviation.

A further development option for this seaplane was the US-2. It differs from the US-1A in cockpit glazing and an updated composition of onboard equipment. The aircraft was equipped with new Rolls-Royce AE 2100 turboprop engines with a capacity of 4500 kW. The design of the wings with integrated fuel tanks was changed. Also, the search and rescue version has a new Thales Ocean Master radar in the bow. A total of 14 US-2 aircraft were built, five aircraft of this type are operated in naval aviation.

By the end of the 60s, the Japanese aviation industry had accumulated considerable experience in the licensed construction of foreign models of aircraft. The design and industrial potential of Japan at that time made it possible to design and build independently aircraft equipment that was not inferior in basic parameters to world standards.

In 1966, Kawasaki, the main contractor in the Nihon Airplane Manufacturing Company (NAMC) consortium, began developing a twin-engine jet military transport aircraft (MTA) based on the terms of reference of the Japan Air Self-Defense Force. The projected aircraft, intended to replace obsolete American-made piston transport aircraft, received the designation C-1. The first of the prototypes took off in November 1970, and flight tests were completed in March 1973.

The aircraft is equipped with two JT8D-M-9 turbojet engines located in engine nacelles under the wing of the American company Pratt-Whitney, manufactured in Japan under license. On-board radio-electronic equipment S-1 allows you to fly in difficult meteorological conditions at any time of the day.

C-1 has a design common to modern transporters. The cargo compartment is pressurized and equipped with an air conditioning system, and the tail ramp can be opened in flight for landing and dropping cargo. The C-1 crew consists of five people, and a typical load includes either 60 fully equipped infantrymen, or 45 paratroopers, or up to 36 stretchers for the wounded with escorts, or various equipment and cargo on landing platforms. Through the cargo hatch located in the tail section of the aircraft, the following can be loaded into the cabin: a 105-mm howitzer or a 2.5-ton truck, or three off-road vehicles.

In 1973, an order was received for the first batch of 11 cars. The upgraded and modified version based on operating experience received the designation C-1A. Its production was completed in 1980, a total of 31 machines of all modifications were built. The main reason for the cessation of production of the C-1A was pressure from the United States, which saw the Japanese transport as a competitor to their C-130.

Despite the "defensive focus" of the Self-Defense Forces, an inexpensive fighter-bomber was required to provide air support to Japanese ground units.

At the beginning of the 70s, the SEPECAT Jaguar began to enter service with European countries, and the Japanese military expressed a desire to have an aircraft of a similar class. Just at the same time, Mitsubishi was developing the T-2 supersonic training aircraft in Japan. It first flew in July 1971, becoming the second Japanese-designed jet trainer and the first Japanese supersonic aircraft.


Japanese TCB T-2

The T-2 aircraft is a monoplane with a high swept wing of variable sweep, an all-moving stabilizer and a single-keel vertical tail unit.

A significant part of the components on this machine were imported, including R.B. 172D.260-50 "Adur" by Rolls-Royce and Turbomeca with a static thrust of 20.95 kN without forcing and 31.77 kN with forcing each, manufactured under license by Ishikawajima. In total, 90 aircraft were manufactured from 1975 to 1988, of which 28 were unarmed T-2Z trainers, and 62 were T-2K combat trainers.

The aircraft had a maximum takeoff weight of 12,800 kg, a maximum speed at altitude of 1,700 km/h, and a ferry range with a PTB of 2,870 km. The armament consisted of a 20 mm cannon, rockets and bombs on seven suspension points, weighing up to 2700 kg.

In 1972, Mitsubishi, commissioned by the Air Self-Defense Forces, began developing the F-1 combat single-seat fighter-bomber based on the T-2 TCB, the first Japanese combat aircraft of its own design since World War II. By design, it is a copy of the T-2 aircraft, but has a single-seat cockpit and more advanced sighting and navigation equipment. The F-1 fighter-bomber made its first flight in June 1975, and serial production began in 1977.

The Japanese aircraft conceptually repeated the Franco-British Jaguar, but could not even come close to it in terms of the number of built ones. A total of 77 F-1 fighter-bombers were delivered to the Air Self-Defense Force. For comparison: SEPEKAT "Jaguar" produced 573 aircraft. The last F-1 aircraft were withdrawn from service in 2006.

The decision to build a training aircraft and a fighter-bomber on the same base was not very successful. As an aircraft for the training and training of pilots, the T-2 turned out to be very expensive to operate, and its flight characteristics did not meet the requirements for a trainer. The F-1 fighter-bomber, while similar to the Jaguar, was seriously inferior to the latter in combat load and range.

According to materials:
Encyclopedia of Modern Military Aviation 1945-2002 Harvest, 2005.
http://www.defenseindustrydaily.com
http://www.hasegawausa.com
http://www.airwar.ru

Aviation of Japan in the Second World War. Part one: Aichi, Yokosuka, Kawasaki Andrey Firsov

Japanese Army Aviation

Japanese Army Aviation

The Japanese army gained its first flight experience back in 1877 using balloons. Later, during the Russo-Japanese War near Port Arthur, two Japanese balloons made 14 successful reconnaissance ascents. Attempts to create devices heavier than air were made by private individuals as early as 1789 - mostly muscle cars, but they did not attract the attention of the military. Only the development of aviation in other countries in the early years of the 20th century caught the attention of Japanese officials. On July 30, 1909, a research organization for military aeronautics was established on the basis of the University of Tokyo and the personnel of the army and navy.

In 1910, the "society" sent Captain Yoshitoshi Tokugawa to France, and Captain Kumazo Hino to Germany, where they were to acquire and master aircraft control. The officers returned to Japan with the Farman biplane and the Grade monoplane, and on December 19, 1910, the first flight of the aircraft in Japan took place. During 1911, when Japan had already acquired several types of aircraft, Captain Tokugawa designed an improved version of the Farman aircraft, which was built by the army aeronautical unit. After training a few more pilots abroad, they began training flights in Japan itself. Despite the training of a fairly large number of pilots and their training in 1918 in the French Air Force, Japanese army pilots did not participate in the battles of the First World War. However, during this period, Japanese aviation had already acquired the appearance of a separate branch of the armed forces - an air battalion was created as part of the army transport command. In April 1919, the unit had already become a division under the command of Major General Ikutaro Inouye.

As a result of a trip to France by the mission of Colonel Faure, which included 63 experienced pilots, several aircraft were acquired that gained fame during the battles of the First World War. Thus, the SPAD S.13C-1 was adopted by the Japanese Imperial Army, the Nieuport-24C-1 was produced by Nakajima as a training fighter, and the Salmson 2A-2 reconnaissance aircraft was built on Kawasaki under the designation "Otsu type 1". Several machines, including the Sopwith "Pap" and "Avro" -504K, were purchased from the UK.

By May 1, 1925, an army air corps was organized, which finally elevated aviation to a military branch along with artillery, cavalry and infantry. Lieutenant General Kinichi Yasumitsu was placed at the head of the air headquarters of the corps ("Koku Hombu"). By the time the air corps was organized, it included 3,700 officers and up to 500 aircraft. Almost immediately after this, the first Japanese-designed aircraft began to enter the corps.

During the first decade of the existence of the air division, and then the corps, he took an insignificant part in the battles in the Vladivostok region in 1920 and in China in 1928 during the "Qingyang Incident". However, over the next decade, the Army Air Forces already played a significant role in the numerous conflicts unleashed by Japan. The first of these was the occupation of Manchuria in September 1931, and in January 1932, the "Shanghai Incident". By this time, the army's air force already had several types of Japanese-designed aircraft in service, including the Mitsubishi Type 87 light bomber, the Kawasaki Type 88 reconnaissance aircraft, and the Nakajima Type 91 fighter. These aircraft allowed the Japanese to easily gain superiority over the Chinese. As a result of these conflicts, the Japanese organized the puppet state of Manchukuo. Since that time, the Japanese Army Aviation has launched an extensive program of modernization and expansion of its forces, leading to the development of many of the types of aircraft with which the Japanese entered the Second World War.

During this rearmament program, on July 7, 1937, fighting resumed in China, which escalated into a full-scale war - "the second Sino-Japanese incident." In the initial period of the war, army aviation was forced to give up leadership in conducting the main offensive operations of the aviation of its eternal rival, the fleet, and limited itself only to covering ground units in the Manchuria region, forming new units and subunits.

By this time, the main unit of army aviation was an air regiment - "hiko rentai", consisting of fighter, bomber and reconnaissance (or transport) squadrons ("chutai"). The first experience of fighting in China required the reorganization of units, and a specialized, smaller unit was created - a group ("sentai"), which became the basis of Japanese aviation during the Pacific War.

Sentai usually consisted of three chutais with 9-12 aircraft and a headquarters unit - "sentai hombu". The group was led by a lieutenant commander. Sentai united in air divisions - "hikodan" under the command of a colonel or major general. Typically, the Hikodan consisted of three sentai in various combinations of "sentoki" (fighter), "keibaku" (light bomber) and "yubaku" (heavy bomber) units. Two or three hikodan were "hikosidan" - the air army. Depending on the needs of the tactical situation, separate subunits of a smaller composition than the sentai were created - "dokuri dai shizugo chutai" (separate squadron) or "dokuri hikotai" (separate air wings).

The high command of the army aviation was subordinated to the "daikhonei" - the imperial supreme headquarters and directly to the "sanbo soho" - the chief of staff of the army. Subordinate to the chief of staff was "koku sokambu" - the highest aviation inspection (responsible for the training of flight and technical personnel) and "koku hombu" - air headquarters, which, in addition to combat control, were responsible for the development and production of aircraft and aircraft engines.

With the arrival of new aircraft of Japanese design and production, as well as the training of flight personnel, the aviation of the imperial army was increasingly used in battles in China. At the same time, Japanese army aviation twice participated in short-term conflicts with the Soviet Union near Khasan and Khalkhin Gol. The clash with Soviet aircraft had a serious impact on the views of the Japanese army. In the eyes of the army headquarters, the Soviet Union became the main potential adversary. With an eye to this, requirements for new aircraft and equipment were developed and military airfields were built along the border with Transbaikalia. Therefore, the air staff first of all demanded from the aircraft a relatively short flight range and the ability to operate in severe frosts. As a result, army planes turned out to be completely unprepared for flights over the expanses of the Pacific Ocean.

During the planning of operations in Southeast Asia and the Pacific, army aviation, due to its technical limitations, had to primarily operate over the mainland and large islands - over China, Malaya, Burma, the East Indies and the Philippines. By the beginning of the war, army aviation from the available 1,500 aircraft allocated 650 to the 3rd Hikosidan for an attack on Malaya and to the 5th Hikosidan, operating against the Philippines.

3rd hikosidan included:

3rd hikodan

7th hikodan

10th hikodan

70th Chutai - 8 Ki-15;

12th hikodan

15th hikotai

50 Chutai - 5 Ki-15 and Ki-46;

51st Chutai - 6 Ki-15 and Ki-46;

83rd hikotai

71st Chutai - 10 Ki-51s;

73rd Chutai - 9 Ki-51s;

89th Chutai - 12 Ki-36;

12th Chutai - Ki-57

5th hikosidan included:

4th hikodan

10th hikotai

52nd Chutai - 13 Ki-51s;

74th Chutai - 10 Ki-36s;

76th Chutai - 9 Ki-15s and 2 Ki-46s;

11th Chutai - Ki-57.

During the first nine months of the war, the aviation of the Japanese army achieved impressive success. Only in Burma did the British pilots and American volunteers meet with rather serious resistance. With the growth of Allied resistance on the borders of India, the Japanese offensive stalled by July 1942. During the battles of this period, Japanese pilots proved themselves well in battles with the "collection" of aircraft samples that the Allies had collected in the Far East.

From the autumn of 1942 to October 1944, the Japanese army was embroiled in a war of attrition, suffering ever-increasing losses in the battles in New Guinea and China. Despite the fact that the Allies gave priority to the war in Europe, during these two years they managed to achieve a numerical superiority of their aircraft in Asia. There they were opposed by all the same aircraft of the Japanese army, developed before the war and already rapidly aging. The Japanese did not have to wait for the arrival of modern cars in large numbers. This was especially true for bombers. Both the Mitsubishi Ki-21 and the Kawasaki Ki-48 had too little bomb load, weak armament, and an almost complete lack of armor protection for the crew and tank protection. The fighter units that received the Ki-61 Hien were in a slightly better position, but the army's fighter aviation was still based on the poorly armed and low-speed Ki-43 Hayabusa. Only the reconnaissance officer Ki-46 was up to the task.

By October 1944, as the war entered a new phase and the Allies landed in the Philippines, the Japanese army began to receive modern Mitsubishi Ki-67 bombers and Nakajima Ki-84 fighters. New machines could no longer help the Japanese in the face of the overwhelming numerical superiority of the Allied aviation, defeats followed one after another. In the end, the war came to the doorstep of Japan itself.

The raids on the Japanese Islands began on June 15, 1944, first from bases in China, then from the Pacific Islands. The Japanese army was forced to deploy numerous fighter units to protect the metropolis, but all available Ki-43, Ki-44, Ki-84, Ki-61 and Ki-100 fighters did not have the necessary flight performance to effectively counter the raids " Superfortresses". In addition, Japanese aviation turned out to be completely unprepared to repel night raids. The twin-engine Kawasaki Ki-45 turned out to be the only acceptable night fighter, but the lack of a locator and low speed made it ineffective. All this was superimposed by a constant shortage of fuel and spare parts. The Japanese command saw a way out in the use of a fairly large mass of obsolete aircraft in suicidal (tayatari) kamikaze sorties, which were first used in the defense of the Philippines. The capitulation of Japan put an end to all this.

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AVIATION In an even sadder situation was the satisfaction of the needs of the Russian army in aviation. There was no production of aircraft engines in peacetime in Russia, except for the branch of the Gnoma plant in Moscow, which produced no more than 5 engines of this kind

Organized on the whole according to the European model, nevertheless, it had unique features. Since the army and navy of Japan had their own aviation, the Air Force as a separate branch of the armed forces, like the German Luftwaffe or the Royal Air Force of Great Britain, did not exist in Japan.

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Air divisions (Hikosidan) - the largest tactical units - reported directly to the headquarters of the Air Armies. In turn, the headquarters of the air divisions exercised command and control of smaller units.

The air brigades (Hikodan) were lower level tactical formations. Usually, one division included two or three brigades. Hikodans were mobile combat formations with a small headquarters, operating at the tactical level. Each brigade usually consisted of three or four Hikosentai (fighter regiment or air group).

Hikosentai, or simply Sentai, was the main combat unit of the Japanese army aviation. Each sentai consisted of three or more chutais (squadrons). Depending on the composition, there were from 27 to 49 aircraft in the sentai. Each Chutai had about 16 aircraft and a corresponding number of pilots and technicians. Thus, the personnel of sentai numbered about 400 soldiers and officers.

A flight (Shotai) usually consisted of three aircraft and was the smallest unit in Japanese aviation. At the end of the war, as an experiment, the number of shotai was increased to four aircraft. But the experiment failed - the fourth pilot invariably turned out to be superfluous, fell out of action and became easy prey for the enemy.

Aviation of the Japanese Imperial Navy

The main organizational and staffing unit of Japan's naval aviation was the air group - kokutai (in army aviation - sentai). As part of naval aviation, there were about 90 air groups, 36-64 aircraft each.

The air groups had numbers or their own names. The names were given, as a rule, according to the base airfield or air command (air groups Iokosuka, Sasebo, etc.). With rare exceptions (Tainan air group), when the air group was transferred to overseas territories, the name was replaced by a number (Kanoya air group, for example, became the 253rd air group). Numbers between 200 and 399 were reserved for fighter air groups, between 600 and 699 for combined air groups. Hydroaviation air groups had numbers between 400 and 499. Deck air groups bore the names of aircraft carriers (Akagi air group, Akagi fighter squadron).

Each air group had three or four squadrons (hikotai), 12-16 aircraft each. A squadron could be commanded by a lieutenant or even an experienced senior non-commissioned officer.

Most of the pilots were sergeants, while in the Allied Air Force almost all pilots were officers. In communication with each other, the sergeants-pilots gave subordination to oblivion, but an abyss lay between the sergeants and officers.

The lowest unit of Japanese aviation was a link of three or four aircraft. For a long time, the Japanese flew in threes. In 1943, Lieutenant Zeinjiro Miyano was the first to copy the Western tactics of fighting in pairs. As a rule, experienced veterans were appointed as leading pairs in a link of four aircraft, and newcomers were appointed as wingmen. This distribution of seats in the link allowed young pilots to gradually gain combat experience and reduce losses. By 1944, Japanese fighters practically stopped flying in threes. A link of three aircraft quickly fell apart in an air battle (it was difficult for the pilots to keep the formation), after which the enemy could shoot down the fighters one by one.

Camouflage and identification designations of Japanese aircraft

Since the beginning of the war in the Pacific, most combat aircraft of army aviation were either not painted at all (they had the color of natural duralumin), or were painted with light gray, almost white, paint. However, already during the war in China, some types of aircraft, for example, the Mitsubishi Ki 21 and Kawasaki Ki 32 bombers, received the first samples of camouflage: on top, the aircraft was painted in uneven stripes of olive green and brown with a narrow white or blue dividing line between them, and on the bottom light gray paint.

With the entry of Japan into the Second World War, the urgency of using camouflage was such that at first it was taken up by the service personnel of aviation units. Most often, the aircraft was covered with spots or stripes of olive green paint at a distance, they merged, providing satisfactory concealment of the aircraft against the background of the underlying surface. Then camouflage coloring began to be applied already in the factory. The most common in this case was the following color scheme: olive green of the upper planes and light gray or natural metal colors of the lower ones. Often the olive-green coloring was applied in the form of separate spots in the form of a "field" coloring. In this case, usually black or dark blue anti-reflective paint was applied on top of the nose.

Experienced and training machines were painted on all surfaces in orange, they had to be clearly visible in the air and on the ground.

The so-called "combat stripes" around the rear fuselage in front of the empennage were used as identification marks. Sometimes they were also applied to the wings. In the last two years of the war, they also included the yellow coloring of the leading edges of the wings to about the middle of the console. But in general, the camouflage schemes for aircraft of the Japanese army aviation often differed from the generally accepted ones and were quite diverse.

Red circles "hinomaru" were used as signs of nationality. They were applied on both sides of the rear fuselage, on the upper and lower planes of the wings. On biplanes, "hinomaru" was applied on the upper planes of the upper wing and the lower planes of the lower pair of wings. On camouflaged aircraft, the Hinomaru usually had a white trim, and sometimes a thin red one as well. On Japanese air defense aircraft, "hinomaru" was applied on white stripes on the fuselage and on the wings.

As the Sino-Japanese War developed, Japanese aircraft began to use markings of individual parts, usually quite colorful. It was either an artistic depiction of a sentai number or a hieroglyph of the first syllabary in the name of the base airfield, or a conventional sign like an arrow. Images of animals or birds were rarely used. Usually, these signs were first applied to the rear of the fuselage and empennage, and then only to the fin and rudder. At the same time, the color of the sign of the unit indicated belonging to a particular unit. So, the headquarters link had a cobalt-blue color of the badge, and 1, 2, 3 and 4 chutai, respectively, were white, red, yellow and green. In this case, the sign often had a white border.

Fleet aircraft also at the beginning of the war in China had a light gray color or the color of natural duralumin. Later, they received sky gray or camouflage dark green and yellow-brown coloration on the upper planes and light gray on the lower planes. True, by the beginning of the war in the Pacific, Japanese naval aircraft were mostly not painted at all and had the color of duralumin.

With the entry of Japan into the Second World War, it was decided to introduce camouflage for torpedo bombers, flying boats and seaplanes. On them, the upper planes were painted in dark green, and the lower planes were painted in light gray, light blue, or had the color of natural metal. Since carrier-based aircraft retained their sky-gray color, when they were relocated to coastal airfields, service personnel applied dark green spots on top of them. At the same time, the intensity of such coloration was quite different: from a barely noticeable "greening", for example, of a keel, to an almost complete dark green coloration.

However, in July 1943, a single solid dark green color of the upper planes was introduced for all combat aircraft of naval aviation.

Experimental and training aircraft were painted orange on all planes, but as the war approached the coast of Japan, the upper planes began to be covered with a dark green color, while the lower planes remained orange. At the very end of the war, all these aircraft received full "combat" camouflage coloring.

In addition, it was common practice for aircraft with an air-cooled engine to paint the hood black, although on some types (Mitsubishi G4M and J2M it was practically not used.

With the outbreak of war, the "combat" stripes on the tails of the fleet's vehicles were painted over, but the yellow coloring of the leading edges of the wings, similar to army aircraft, remained.

The Hinomaru nationality insignia was modeled on the army, but on naval air defense aircraft, in contrast to the army, white stripes were not applied under them. True, sometimes "hinomaru" was applied in white or yellow squares.

Part designations were applied to the keel and stabilizer of the aircraft. At the beginning of the war, one or two hieroglyphs of the syllabic letter "Kana" were applied to the keel, usually denoting the name of the base in the metropolis to which the aircraft was assigned. If the aircraft was on one or another theater of operations, it received a Latin letter or even a Latin numeral for carrier-based aircraft. The designation of the part through a hyphen was usually followed by a three-digit number of the aircraft itself.

In the middle of the war, the alphanumeric designation system was replaced with a purely digital one (two to four digits). The first digit usually meant the nature of the unit, the other two meant its number, then, through a hyphen, the usually two-digit number of the aircraft itself also followed. And, finally, by the end of the war, since many units were concentrated in Japan, they again returned to the alphanumeric notation.

Japanese aircraft designation system

During the Second World War, the Japanese Air Force used several aircraft designation systems at once, which completely confused Allied intelligence. So, for example, the aircraft of the Japanese army aviation usually had the number "china" (designs) for example Ki 61, the type number "army type 3 fighter" and the proper name Hien. To simplify identification, the Allies introduced their own aircraft code designation. So, Key 61 became "Tony".

Initially, for about 15 years of its existence, the Japanese army aviation used several aircraft designation systems at once, mainly adopting factory designations. But by the beginning of World War II, none of the aircraft with these notation systems had survived.

In 1927, a system of type numbers was introduced, which was used until the very defeat of Japan. In parallel, since 1932, the system of numbers "China" (design number NN) began to be used. In addition, some aircraft received their own names. Special notation systems were used to designate experimental aircraft, autogyros and gliders.

Since 1932, all Japanese army aircraft have received a continuous numbering "China", including the types already adopted for service. The end-to-end numbering "China" was retained until 1944, when, in order to mislead the Allied intelligence, it became arbitrary. In addition to the "China" number, the aircraft received Roman numerals designating different models. Aircraft of the same model, in addition, differed depending on the modifications and an additional letter of one of the Japanese alphabets: the first modification was called "Ko", the second "Otsu", the third "Hei" and so on (these hieroglyphs did not mean any particular digital or alphabetical order of calculation, rather they corresponded to the notation "north" "east" "south" "west"). Recently, not only in the West, but also in Japanese aviation literature, it is customary to put a Latin letter instead of the corresponding Japanese character after Roman numerals. Sometimes, in addition to the numerical and alphabetic designation of modifications and models, the abbreviation KAI (from "Kaizo" modified) was also used. It is customary to designate the design number abroad with the letters "Ki", ​​however, in Japanese documents, the English Ki was never used, but the corresponding hieroglyph was used, so we will use the Russian abbreviation Ki in the future.

As a result, for example, for the line of the Hien Ki 61 fighter, such a notation looked like this:

Ki 61 - the designation of the project and the prototype
Key 61-Ia - the first production model "Hiena"
Ki 61-Ib - a modified version of the production model "Hiena"
Ki 61-I KAIS - the third version of the first production model
Ki 61-I KAID - the fourth version of the first production model
Ki 61-II - experimental aircraft of the second production model
Ki 61-II KAI - modified experimental aircraft of the second production model
Ki 61-II KAIA - the first version of the second production model
Ki 61-II KAIB - the second version of the second production model
Ki 61-III - project of the third production model

For gliders, the designation "Ku" (from "Kuraida" glider) was used. For some types of aircraft, brand designations were also used (for example, for the Kayabe Ka 1 autogyro). There was a separate designation system for missiles, but the Kawanishi Igo-1-B sample was also called Ki 148 in order to disorient Allied intelligence.

In addition to the "China" numbers, army aviation also used numbering according to the years the model was put into service, which included a short designation of the aircraft's purpose. The numbering was carried out according to the Japanese system of chronology, while the last two digits were taken. So, an aircraft put into service in 1939 (or in 2599 according to the Japanese calendar) became "type 99", and put into service in 1940 (that is, in 2600) "type 100".

Thus, the aircraft put into service in 1937 received such a long designation: Nakajima Ki 27 "fighter army type 97"; Mitsubishi Ki 30 "army type 97 light bomber"; Mitsubishi Ki 21 "heavy bomber army type 97"; Mitsubishi Ki 15 "strategic reconnaissance army type 97". The designation of the purpose of the aircraft helped to avoid confusion, for example, for two "types 97" of the Mitsubishi Ki 30 single-engine bomber and the Ki 21 twin-engine bomber of the same company. True, sometimes two types of aircraft of the same purpose were put into service in one year. For example, in 1942, the Ki 45 KAI twin-engine fighter and the single-engine Ki 44 fighter were adopted. In this case, the Ki 45 became the "army type 2 two-seat fighter", and the Ki 44 "military type 2 single-seat fighter."

For various modifications of aircraft in a long system of designations, the model number was additionally assigned with an Arabic numeral, the serial version number and a Latin letter, the modification number of this serial model. As a result, in relation to the numbering "China", the long designation looked like this:

Ki 61 - before the adoption of the aircraft, the type number was not assigned
Ki 61-Ia - Army type 3 fighter model 1A (type 3 by year 2603)
Ki 61-Ib - army type 3 fighter model 1B
Ki 61-I KAIS - army type 3 fighter model 1C
Ki 61-I KAId - army type 3 fighter model 1D
Ki 61-II - again, the experimental aircraft does not have type numbers
Key 61-II KAI - no
Ki 61-II KAIA - army type 3 fighter model 2A
Ki 61-II KAIb - army type 3 fighter model 2B
Ki 61-III - experimental aircraft, no type number

For foreign aircraft, the abbreviation of the name of the country of manufacture and the native company was used as a type designation. For example, the Fiat BR.20 was designated "heavy bomber type 1" and the transport aircraft Lockheed "type LO".

In addition to these two designation systems, since the entry of Japan into World War II, aircraft have received short nicknames. The reason for this was, on the one hand, the clear readability for the allied intelligence of a long name to determine the type of aircraft and its purpose, on the other hand, the difficulty of using a long designation in a combat situation, for example, when talking over the radio. In addition, the catchy names of the aircraft were to be used in promoting the actions of their own aviation among the population of Japan. Moreover, if the fleet followed a certain system when assigning such names, then the army assigned them completely arbitrarily.

In addition, in a combat situation, abbreviations of the long name of the aircraft were used, which became widely known, but nevertheless rarely used in the future. So, "strategic reconnaissance army type 100" was also called "Sin-City" and "attack aircraft type 99" "Guntei".

In turn, by the beginning of the Pacific War, the aviation of the Japanese fleet had as many as three aircraft designation systems: "C" numbers, "type" numbers and a "short" designation. Later during the war, the fleet began to use two more ways to designate aircraft, now they used their own names and a special designation system developed by the fleet aviation bureau.

The designation system for experimental aircraft "C" was used for all experimental aircraft commissioned by the fleet, starting in 1932, the seventh year of the reign of Emperor Hirohito. Therefore, the aircraft developed under the aircraft construction program of this year were called 7-Si, and the developments of 1940 were called 15-Si. In order to distinguish between different aircraft created under the same program, a description of the purpose of the aircraft was used (carrier-based fighter, reconnaissance seaplane, etc.). As a result, for example, the full designation of the 1932 seaplane developed by Kawanishi was: "experimental reconnaissance seaplane 7-Ci." This notation, similar to the British, was used until the end of the war.

In addition, at the end of the 30s, the fleet adopted a short aircraft designation system, similar to that used by the US Naval Aviation until 1962, an alphanumeric combination. The first letter indicated the purpose of the aircraft:

A - carrier-based fighter
B - torpedo bomber
C - carrier-based reconnaissance aircraft
D - deck dive bomber
E - reconnaissance seaplane
F - patrol seaplane
G - coastal bomber
H - flying boat
J - coastal fighter
K - training aircraft
L - transport aircraft
M - "special" aircraft
MX - aircraft for special missions
N - float fighter
P - bomber
Q - patrol aircraft
R - coastal reconnaissance
S - night fighter

This was followed by a number indicating the procedure for adopting this type into service; it was assigned when the aircraft development program was launched. Then came the letter combination, denoting the company that developed the aircraft. At the end was the model number of this aircraft. Minor modifications made to the car were indicated by a Latin letter.

In addition, if an aircraft changed its designation during its life cycle, then a letter of the corresponding type of aircraft followed through a hyphen. So, the training version of the aircraft received, for example, the designation B5N2-K.

Foreign-designed aircraft in place of the manufacturer's letter received the abbreviated name of their company (for Heinkel, for example, A7Nel), and if the aircraft was purchased for experimental purposes, then instead of the number there was the letter X, that is, AHNel).

In the fleet, the following abbreviations of the names of the developer companies were used:

A - Aichi and North American
B - Boeing
C - Consolidated
D - Douglas
G - Hitachi
N - Hiro and Hawker
Not - Heinkel
J - Nipon kagata and Junkers
K - Kawanishi and Kinnear
M - Mitsubishi
N - Nakajima
R - Nihon
S - Sasebo
Si - Owl
V - Vout-Sikorsky
W - Watanabe, later Kyushu
Y - Yokosuka
Z - Mizuno

Since 1921, for most aircraft produced in Japan, the Navy has used a long designation of the aircraft, which included a brief description of its purpose and type number. From 1921 to 1928, numbers were used indicating the year of the era of the next emperor, that is, from 1921 to 1926 numbers from 10 to 15, and in 1927-28 2 and 3. However, after 1929, the last two digits of the current year were used according to the Japanese calendar. For the year 2600 (that is, 1940), the designation "type 0" was obtained (in the army, if you remember, "type 100").

To designate various modifications of the same type of aircraft, the model number was used in the long designation: initially one digit (for example, "model 1") or through a hyphen also the revision number ("model 1-1"). Since the late 30s, changes have been made to the numbering of models; it has become two-digit. The first digit now meant the serial number of the modification, and the second the installation of a new motor. So, "model 11" meant the first serial modification, "model 21" the second serial modification with the same engine, and "model 22" the second modification with a new type of engine. Additional improvements within the same modification were indicated by the character of the Japanese alphabet: "Ko" the first, "Otsu" the second, "Hei" the third. Usually they were replaced by the letter of the Latin alphabet corresponding in order, that is, the Mitsubishi A6M5s or "carrier-based bomber marine type 0 model 52-Hei" was also written "model 52C".

A similar long designation was used for foreign-designed aircraft, with the type number replaced by the abbreviated name of the company, that is, the Heinkel A7Nel had a long designation of the He air defense fighter.

At the end of 1942, the long designation system was changed in order to preserve the secrecy of the purpose of the aircraft: it now included the code designation of the aircraft. Prior to that, relatively few aircraft proper names that had become generally accepted had taken root in fleet aviation. So, the Mitsubishi G4M1 bomber was nicknamed "Hamaki" (Cigar). However, in July 1943, the fleet revised the aircraft designation system and began to add the aircraft's own name to the long name. In this case, the name of the aircraft was chosen according to the following principle:

fighters were designated by the names of weather phenomena - deck and hydrofighters were baptized by the names of the winds (the names ended in fu)
air defense fighters - variations on the theme of lightning (ended in den)
night fighter names ended in ko (light)
attack aircraft were designated by the names of mountains
scouts were called different clouds
bombers - by the names of stars (s) or constellations (zan)
patrol planes - by the names of the oceans
training machines - names of various plants and flowers
auxiliary aircraft were called elements of the landscape

In 1939, the Fleet Aviation Bureau launched a program to improve the aviation service, under which design teams received certain requirements and project development conditions for submission to the fleet aviation before receiving an order for a full-scale design. Aircraft projects that took these requirements into account received a special design designation, consisting of an abbreviation of the company name, like a short designation, and a two-character number (10, 20, 30, etc.). True, the specific numbers of the projects that were worn by certain aircraft were buried along with the documentation destroyed before the surrender of Japan.

The allies, who had little understanding of the designation system for Japanese aircraft and often did not know what this or that aircraft was actually called, starting somewhere in the second half of 1942, began to give Japanese aircraft various nicknames. At first, all the planes that were fighters were called "Zero", and all that dropped bombs were called "Mitsubishi". To put an end to various misunderstandings, the Allied Air Technical Intelligence Service was asked to clean up the matter.

The official Japanese aircraft designations, if they became known to the Allies, were of little help. Tried to use them for lack of anything better. They also tried to use the names of manufacturers to designate aircraft, but this led to confusion if the aircraft was produced by several companies at once.

In June 1942, American intelligence captain Frank McCoy, sent as an intelligence officer to Australia, organized an enemy materiel section as part of the Allied Air Force Intelligence Directorate in Melbourne. McCoy had only two men at his disposal, Sergeant Francis Williams and Corporal Joseph Grattan. It was they who were tasked with identifying Japanese aircraft. McCoy himself described his work as follows:

“In order to identify Japanese aircraft, the urgent task immediately arose to introduce some kind of classification of them, and we decided to start by adopting our own system for codifying enemy aircraft. Since I myself am from Tennessee, we used various village nicknames Zeke, Nate, Roof, Jack , Reet is simple, short and easy to remember.Sergeant Williams and I gave rise to these nicknames in numerous disputes, and began to use our aircraft codes from July 1942. This work received the full support of the head of the intelligence service, Commodore of the British Royal Air Force Hewitt and his deputy Major of the American Air Force Ben Kane, and they offered to urgently finish this work. I told them that I was already working like a man possessed, because everyone around him thought we were crazy. In the first month alone, we assigned 75 codes."

Thus, most of the designations of Japanese aircraft used by the Allied air forces appeared. By September 1942, the intelligence of the southwestern sector of the Pacific began to prepare information using this notation. Soon sheets with silhouettes and code names of Japanese aircraft began to arrive in the South Pacific and Burma. McCoy meanwhile began to seek from Washington and the Air Ministry in London the standardization of this or a similar system of codification. His requests were initially met with incomprehension, once even McCoy was called to explain to General MacArthur: it turned out that one of the code designations "Hap" was the nickname of the Chief of Staff of the American Army, General Henry Arnold, and "Jane" (the code designation for the most common Japanese bomber, Ki 21) turned out to be the name of MacArthur's own wife. At the end of 1942, the code designation system for Japanese aircraft was adopted by the US Air Force and the Navy and Marine Corps, and a few months later by the British Air Ministry.

After that, McCoy's section was already officially given the task of codifying all new Japanese aircraft. At the same time, code designations were assigned randomly, but in the summer of 1944 the joint air center in Anacostia took over this task and introduced the following code assignment principle: Japanese fighters of all types received male names; bombers, reconnaissance and transport aircraft are female (transport with the letter T), training machines are the names of trees, and gliders are birds. True, there were exceptions to the rule. Thus, the Nakajima Ki 44 fighter, which had already received the nickname "Tojo" in China after the then Prime Minister of Japan, retained this code designation by common consent.

The aircraft was produced by Kawasaki in 1935-1938. It was an all-metal biplane with fixed landing gear and an open cockpit. A total of 588 cars were produced, incl. Ki-10-I - 300 vehicles and Ki-10-II - 280 vehicles. TTX machines: length - 7.2 m; height - 3 m; wingspan - 10 m; wing area - 23 m²; empty weight - 1.4 tons, take-off - 1.7 tons; engine - Kawasaki Ha-9 with a power of 850 hp; rate of climb - 1,000 m / m; maximum speed - 400 km / h, practical range - 1,100 km; practical ceiling - 11,500 m; armament - two 7.7 mm Type 89 machine guns; crew - 1 person.

The night heavy fighter was produced by Kawasaki in 1942-1945. A total of 1.7 thousand vehicles were produced in four serial modifications: Ki-45 KAIa, Ki-45 KAIb, Ki-45 KAIc and Ki-45 KAId. TTX machines: length - 11 m; height - 3.7 m; wingspan - 15 m; wing area - 32 m²; empty weight - 4 tons, take-off - 5.5 tons; engines - two Mitsubishi Ha-102 with a capacity of 1,080 hp; the volume of fuel tanks - 1 thousand liters; rate of climb - 11 m / s; maximum speed - 547 km / h; practical range - 2,000 km; practical ceiling - 9,200 m; armament - 37-mm gun No-203, two 20-mm Ho-5, 7.92-mm machine gun Type 98; ammunition 1,050 rounds; bomb load - 500 kg; crew - 2 people.

The aircraft was produced by Kawasaki in 1942-1945. It had an all-metal semi-monoque fuselage structure, pilot armor and protected tanks. In total, 3.2 thousand vehicles were produced in two serial versions: Ki-61-I and Ki-61-II, which differed in equipment and weapons. TTX machines: length - 9.2 m; height - 3.7 m; wingspan - 12 m; wing area - 20 m²; empty weight - 2.8 tons, take-off - 3.8 tons; engine - Kawasaki Ha-140 with a capacity of 1,175 - 1,500 hp; the volume of fuel tanks - 550 l; rate of climb - 13.9 - 15.2 m / s; maximum speed - 580 - 610 km / h, cruising - 450 km / h; practical range - 1,100 - 1,600 km; practical ceiling - 11,000 m; armament - two 20-mm No-5 guns, two 12.7-mm machine guns Type No-103, 1,050 rounds of ammunition; bomb load - 500 kg; crew - 1 person.

The aircraft was produced by Kawasaki based on the Ki-61 Hien in 1945 by replacing the liquid-cooled engine with an air-cooled engine. A total of 395 vehicles were produced in two versions: Ki-100-Ia and Ki-100-Ib. TTX machines: length - 8.8 m; height - 3.8 m; wingspan - 12 m; wing area - 20 m²; empty weight - 2.5 tons, take-off - 3.5 tons; engine - Mitsubishi Ha 112-II with a capacity of 1,500 hp rate of climb - 16.8 m / s; maximum speed -580 km / h, cruising - 400 km / h; practical range - 2,200 km; practical ceiling - 11,000 m; armament - two 20-mm guns No-5 and two 12.7-mm machine guns Type No-103; crew - 1 person.

A twin-engine, two-seat, long-range fighter-interceptor was produced by Kawasaki based on the Ki-96 in 1944-1945. A total of 238 vehicles were built. TTX machines: length - 11.5 m; height - 3.7 m; wingspan - 15.6 m; wing area - 34 m²; empty weight -5 tons, take-off - 7.3 tons; engines - two Mitsubishi Ha-112 with a capacity of 1,500 hp; rate of climb - 12 m / s; maximum speed - 580 km / h; practical range - 1,200 km; practical ceiling - 10,000 m; armament - 57-mm gun No-401, two 20-mm guns No-5 and 12.7-mm machine gun Type No-103; bomb load - 500 kg; crew - 2 people.

The single-seat fighter of all-metal construction "N1K-J Shiden" was produced by Kawanishi in 1943-1945. in two serial modifications: N1K1-J and N1K2-J. A total of 1.4 thousand cars were produced. TTX machines: length - 8.9 - 9.4 m; height - 4 m; wingspan - 12 m; wing area - 23.5 m²; empty weight -2.7 - 2.9 tons, take-off - 4.3 - 4.9 tons; engine - Nakajima NK9H with a power of 1,990 hp; rate of climb - 20.3 m / s; maximum speed - 590 km / h, cruising - 365 km / h; practical range - 1,400 - 1,700 km; practical ceiling - 10,700 m; armament - two 20 mm Type 99 cannons and two 7.7 mm machine guns or four 20 mm Type 99 cannons; bomb load - 500 kg; crew - 1 person.

A single-seat fighter-interceptor of all-metal construction was produced by Mitsubishi in 1942-1945. A total of 621 vehicles of the following modifications were produced: J-2M1 - (8 vehicles), J-2M2 - (131), J-2M3 (435), J-2M4 - (2), J-2M5 - (43) and J- 2M6(2). TTX machines: length - 10 m; height - 4 m; wingspan - 10.8 m; wing area - 20 m²; empty weight - 2.5 tons, take-off - 3.4 tons; engine - Mitsubishi MK4R-A with a power of 1,820 hp; rate of climb - 16 m / s; maximum speed - 612 km / h, cruising - 350 km / h; practical range - 1,900 km; practical ceiling - 11,700 m; armament - four 20-mm guns Type 99; bomb load - 120 kg; crew - 1 person.

A twin-engine night fighter of all-metal construction was produced by Mitsubishi on the basis of the Ki-46 reconnaissance aircraft in 1944-1945. It was a low-winged monoplane with a retractable tailwheel undercarriage. In total, 613 thousand cars were produced. TTX machines: length - 11 m; height - 3.9 m; wingspan - 14.7 m; wing area - 32 m²; empty weight - 3.8 tons, take-off - 6.2 tons; engines - two Mitsubishi Ha-112 with a capacity of 1,500 hp; the volume of fuel tanks - 1.7 thousand liters; rate of climb - 7.4 m / s; maximum speed - 630 km / h, cruising - 425 km / h; practical range - 2,500 km; practical ceiling - 10,700 m; armament - 37 mm cannon and two 20 mm cannons; crew - 2 people.

An all-metal loitering fighter-interceptor was produced by Mitsubishi in 1944 based on the Ki-67 bomber. A total of 22 cars were produced. TTX machines: length - 18 m; height - 5.8 m; wingspan - 22.5 m; wing area - 65.9 m²; empty weight -7.4 tons, take-off - 10.8 tons; engines - two Mitsubishi Ha-104 with a power of 1900 hp; rate of climb - 8.6 m / s; maximum speed - 550 km / h, cruising - 410 km / h; practical range - 2,200 km; practical ceiling - 12,000 m; armament - 75-mm cannon Type 88, 12.7-mm machine gun Type 1; crew - 4 people.

The twin-engine night fighter was produced by Nakajima Aircraft in 1942-1944. A total of 479 vehicles were built in four modifications: J-1n1-C KAI, J-1N1-R (J1N1-F), J-1N1-S and J-1N1-Sa. TTX machines: length - 12.2 - 12.8 m; height - 4.6 m; wingspan - 17 m; wing area - 40 m²; empty weight - 4.5-5 tons, take-off - 7.5 - 8.2 tons; engines - two Nakajima NK1F Sakae 21/22 with a power of 980 - 1,130 hp; rate of climb - 8.7 m / s; fuel tank capacity - 1.7 - 2.3 thousand liters; maximum speed - 507 km / h, cruising - 330 km / h; practical range - 2,500 - 3,800 km; practical ceiling - 9,300 - 10,300 m; armament - two to four 20 mm Type 99 cannons or a 20 mm cannon and four 7.7 mm Type 97 machine guns; crew - 2 people.

The fighter was produced by the Nakajima company in 1938-1942. in two main modifications: Ki-27a and Ki-27b. It was a single-seat all-metal low-wing aircraft with a closed cockpit and fixed landing gear. A total of 3.4 thousand cars were produced. TTX machines: length - 7.5 m; height - 3.3 m; wingspan - 11.4 m; wing area - 18.6 m²; empty weight - 1.2 tons, take-off - 1.8 tons; engine - Nakajima Ha-1 with a power of 650 hp; rate of climb - 15.3 m / s; maximum speed - 470 km / h, cruising - 350 km / h; practical range - 1,700 km; practical ceiling - 10,000 m; armament - 12.7 mm machine gun Type 1 and 7.7 mm machine gun Type 89 or two 7.7 mm machine guns; bomb load - 100 kg; crew - 1 person.

Fighter Nakajima Ki-43 Hayabusa

The aircraft was produced by Nakajima in 1942-1945. It was an all-metal single-engine single-seat cantilever low-wing aircraft. The rear of the fuselage was a single unit with the tail unit. At the base of the wing there were retractable all-metal flaps, increasing not only the curvature of its profile, but also the area. A total of 5.9 thousand vehicles were produced in three serial modifications - Ki-43-I/II/III. TTX machines: length - 8.9 m; height - 3.3 m; wingspan - 10.8 m; wing area - 21.4 m²; empty weight - 1.9 tons, take-off - 2.9 tons; engine - Nakajima Ha-115 with a power of 1,130 hp; rate of climb - 19.8 m / s; the volume of fuel tanks - 563 l; maximum speed - 530 km / h, cruising - 440 km / h; practical range - 3,200 km; practical ceiling - 11,200 m; armament - two 12.7-mm machine guns No-103 or two 20-mm guns Ho-5; bomb load - 500 kg; crew - 1 person.

A single-seat fighter-interceptor of all-metal construction was produced by Nakajima in 1942-1944. It had a semi-monocoque fuselage, a low-lying wing with all-metal flaps equipped with a hydraulic actuator. The pilot's cockpit was covered with a teardrop-shaped lantern of all-round visibility. Tricycle landing gear with two main struts and a tail wheel. All landing gear wheels in flight were removed by a hydraulic system and covered with shields. A total of 1.3 thousand aircraft were produced. TTX machines: length - 8.9 m; height - 3 m; wingspan - 9.5 m; wing area - 15 m²; empty weight - 2.1 tons, take-off - 3 tons; engine - Nakajima Ha-109 with a power of 1,520 hp; the volume of fuel tanks - 455 l; rate of climb - 19.5 m / s; maximum speed - 605 km / h, cruising - 400 km / h; practical range - 1,700 km; practical ceiling - 11,200 m; armament - four 12.7-mm machine guns No-103 or two 40-mm guns Ho-301, 760 rounds of ammunition; bomb load - 100 kg; crew - 1 person.

A single-seat fighter was produced by Nakajima in 1943-1945. in total, 3.5 thousand vehicles were produced in the following modifications: Ki-84, Ki-84-Ia / b / c and Ki-84-II. It was a cantilever low-wing monoplane of all-metal construction. It had pilot armor, armored fuel tanks and retractable landing gear. TTX machines: length - 9.9 m; height - 3.4 m; wingspan - 11.2 m; wing area - 21 m²; empty weight - 2.7 tons, take-off - 4.1 tons; engine - Nakajima Na-45 with a capacity of 1,825 - 2,028 hp; the volume of fuel tanks - 737 l; rate of climb - 19.3 m / s; maximum speed - 630 - 690 km / h, cruising - 450 km / h; practical range - 1,700 km; practical ceiling - 11,500 m; armament - two 20 mm No-5 cannons, two 12.7 mm Type No-103 machine guns or four 20 mm No-5; bomb load - 500 kg; crew - 1 person.



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