Since the end of World War II, the Japanese military-industrial complex has not shone with the “pearls” of its military industry, and has become entirely dependent on the imposed products of the American defense industry, the powerful lobby of which was carried out by the Japanese government 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 modern composition Air Force (or Air Self-Defense Forces): these are 153 units of F-15J (a complete copy of the F-15C), 45 units of F-15DJ (a copy of the two-seat F-15D). On this 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 aircraft are designed to use the AGM-88 “HARM” anti-aircraft missile system.

The rest of the fighter-reconnaissance aircraft, 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F-4EJ, RF-4EJ, EF-4EJ aircraft, of which there are about 80 in the country’s Air Force, now they are gradually being withdrawn from service.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 is accompanied by the latest Russian naval reconnaissance aircraft Tu-214R

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

This most affected the airframe and avionics. The nose of the fuselage is a purely Japanese design using a new geometric idea that differs from the Falcon.

The F-2A boasts a completely new wing with less sweep, but a 1.25 higher aerodynamic lift coefficient (load-bearing property): the wing area of ​​the Falcon is 27.87 m 2, for the F-2 - 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-state 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. This 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 a General Electric F110-GE-129 turbojet afterburner engine with a maximum thrust of 13.2 tons. Note that the capacity of the internal fuel tanks is 4675 liters, and 5678 when 3 more are suspended PTB. The newest American F-16C Block 60 has only 3080 liters in its internal tanks. The Japanese made a very wise move: citing their defensive nature of the aircraft, in case of conflict within only Japan, they made it possible for the F-2A to have more fuel on board and maintain maneuverability on high level, without using massive PTB. Due to this, a higher combat radius of action is about 830 km versus 580 for the Falcon.

The fighter has a service ceiling of more than 10 km, and a flight speed at high altitude of 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 is a strong indicator even today.

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

The radar is capable of “tying up” (SNP) at least 10 target routes, and firing at 4-6 of them. Considering that in the 90s the phased array industry was actively developing in the Russian Federation and other countries, we can judge the operating range of the radar for a “fighter” type target (3 m 2) of no more than 120-150 km. However, at that time, AFAR and PFAR were installed 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 electronic control system, communication devices and data transmission on the tactical situation in the short and ultra-short 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 MFI of tactical information, and two monochrome MFIs - CRT.

The armament is almost identical to the American F-16C, and is represented by AIM-7M, AIM-120C, AIM-9L,M,X missiles; It is worth noting the prospect of the Japanese air-to-air missile AAM-4, 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 promising weapons.

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

Japan is already “stepping” into the 5th generation of fighter aircraft on its own, as evidenced by the Mitsubishi ATD-X “Shinshin” project (“Shinshin” means “soul”).

Japan, like every technological superpower, by definition must have its own stealth air superiority fighter; the start of work on the magnificent descendant of the legendary aircraft A6M “Zero” started back in 2004. We can say that the employees of the Technical Design Institute of the Ministry of Defense have approached the stage of creating components of the new machine in a “different plane”.

Since the Xinxing project received its first prototype much later than the F-22A, and it undoubtedly took into account and eliminated all the shortcomings and mistakes that the Russians, Americans and Chinese learned from, and also absorbed all the best aerodynamic ideas for implementation of ideal performance characteristics, the latest developments in the avionics base, where Japan has already succeeded.

The first flight of the ATD-X prototype is scheduled for the winter of 2014-2015. In 2009, funds in the amount of $400 million were allocated for the development of the program and the construction of an experimental vehicle alone. Most likely, the Sinsin will be called the F-3 and will enter service no earlier than 2025.

Shinshin is the smallest fighter of the fifth generation, however, the expected range is about 1800 km

What do we know about Sinsin today? Japan is a small power and does not plan to independently participate in large regional wars with the Air Self-Defense Forces, sending its combat aircraft thousands of kilometers deep into enemy territories, hence the name Air Self-Defense Forces. Therefore, the dimensions of the new “stealth aircraft” 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 small sizes airframe and the widest use of composite materials, which is more than 30% plastic with reinforcing carbon, 2 low-weight XF5-1 turbofans with a thrust of about 5500 kg/s each, the weight of an empty fighter will be in the range of 6.5-7 tons, i.e. weight and dimensions will be very close to French fighter Mirage-2000-5.

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

The Sinsin engines are equipped with an all-aspect OVT system, consisting of three controlled aerodynamic petals, which look very “oaky”, like for a 5+ generation fighter, but apparently Japanese engineers saw in this design some guarantees of greater reliability than our “all-aspect” one. on product 117C. But in any case, this nozzle is better than the American one installed on , where 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 target detection range of the F-16C type will be about 180 km, close to the Zhuk-A and AN/APG-80 radars, and a multi-channel data transmission bus based on fiber-optic conductors controlled by the most powerful digital computers. Given 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 fuselage length than other aircraft (the Sinsin has 0.62, the PAK-FA has 0.75), an airframe with an aerodynamically load-bearing structure, as well as developed forward overhangs 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 characterized by medium-speed “energy” maneuvering using OVT.

“Three-blade” 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 clear position of complete non-proliferation in the field of “precision” defense, refused to provide the Japanese side with even a “depleted version” of the F-22A.

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

/Evgeny Damantsev/

FOREIGN MILITARY REVIEW No. 9/2008, pp. 44-51

MajorV. BUDANOV

Start see: Foreign military review. - 2008. - No. 8. - P. 3-12.

The first part of the article examined the general organizational structure of the Japanese Air Force, as well as the composition and tasks performed by the air combat command.

Command combat support (KBO) is intended to support the activities of the LHC. It solves the problems of search and rescue, military transport, transport and refueling, meteorological and navigation support. Organizationally, this command includes a search and rescue air wing, three transport air groups, a transport and refueling squadron, air traffic control, meteorological support and radio navigation control groups, as well as a special transport air group. The number of KBO personnel is about 6,500 people.

This year, the first squadron of transport and refueling aviation was created in the KBO with the aim of expanding the operational zone of fighter aircraft and increasing the combat capabilities of the Air Force to protect islands and sea communications remote from the main territory. At the same time, it is expected to increase the duration of fighter aircraft patrols in threatened areas. The presence of refueling aircraft will also make it possible to carry out non-stop transfer of fighters to remote training grounds (including abroad) to practice operational and combat training tasks. Aircraft new to Japanese Air Force class can be used to deliver personnel and cargo and enable greater participation of national armed forces in international peacekeeping and humanitarian operations. It is assumed that refueling aircraft will be based at Komaki Air Base (Honshu Island).

In total, according to the calculations of military department specialists, it is considered advisable to have in the future combat strength Japanese Air Force up to 12 tanker aircraft. Organizationally, the refueling aviation squadron will include a headquarters and three groups: refueling aviation, aviation engineering support and airfield maintenance. The total staffing level of the units is approximately 10 people.

Simultaneously with the performance of refueling functions, the aircraftKC-767 Jintended to be used as a transport

Organizational structure of the Japanese Air Force Combat Support Command

The basis of the squadron being formed will be the KC-767J transport and refueling aircraft (TRA) produced by the American company Boeing. In accordance with the application of the Japanese Ministry of Defense, the United States is converting four already built Boeing 767s into the corresponding modification. One aircraft is valued at approximately $224 million. The KC-767J is equipped with a controlled fuel refueling boom in the rear fuselage. With its help, he will be able to refuel one aircraft in the air with a fuel transfer rate of up to 3.4 thousand l/min. The time required to refuel one F-15 fighter (fuel tank capacity 8 thousand liters) will be about 2.5 minutes. The total fuel supply of the aircraft is 116 thousand liters. Depending on the need, fuel can either be used by the KC-767J itself or transferred to other aircraft. This will allow for more flexible use of the reserves available on board. The capabilities of a vehicle of this type for in-flight refueling can be increased by installing an additional fuel tank with a capacity of about 24 thousand liters in the cargo compartment.

Along with performing refueling functions, the KC-767J aircraft is intended to be used as a transport aircraft for the delivery of cargo and personnel. Conversion from one version to another takes from 3 to 5 hours 30 minutes. The maximum carrying capacity of this vehicle is 35 tons or up to 200 personnel with standard small arms.

In addition to the standard avionics installed on Boeing 767 aircraft, the KC-767J is equipped with a set of equipment special purpose, including: RARO-2 air refueling control system, meter and decimeter radio communications, GATM air traffic control system, friend-foe identification equipment, Link-16 high-speed data transmission equipment, UHF direction-finding station range, TAKAN radio navigation system and NAVSTAR CRNS receiver. According to the KC-767J combat use plan, it is assumed that one TZS will support up to eight F-15 fighters.

Organizational structure of the Japanese Air Force Training Command

Currently, the Japanese Air Force has only three types of aircraft (F-4EJ, F-15J/DJ and F-2A/B fighters) equipped with in-flight refueling systems. In the future, the presence of such systems will be considered as a prerequisite for promising fighter aircraft. The training of Japanese Air Force fighter aircraft to solve the problem of in-flight refueling has been carried out on a regular basis since 2003 during special flight tactical training, as well as joint exercises with the US Air Force "Cope Thunder" (Alaska) and "Cope North" (Alaska). Guam, Mariana Islands). During these activities, the transfer of fuel is worked out jointly with the American fuel station KS-135, based at the Kadena Air Base (Okinawa Island).

At the request of the military department, since 2006, measures have been taken to ensure the possibility of in-flight refueling of helicopters. As part of the allocated allocations of over $24 million, it is planned, in particular, to convert the military transport aircraft (MTC) S-ION into a tanker. As a result, the vehicle will be equipped with a rod for receiving fuel and two devices for transmitting it in the air using the “hose-cone” method, as well as additional tanks. The upgraded C-130N will be able to itself receive fuel from another refueling aircraft and carry out simultaneous mid-air refueling of two helicopters. It is assumed that the volume of fuel reserves will be about 13 thousand liters, and its transmission speed will be 1.1 thousand l/min. At the same time, work began on installing the corresponding equipment on the UH-60J, CH-47Sh and MSN-101 helicopters.

In addition, the Ministry of Defense decided to provide refueling capabilities to the promising C-X transport aircraft. For this purpose, on the second prototype the necessary improvements and research have been carried out. According to the leadership of the military department, this will not affect the already determined deadlines for the implementation of the R&D program, according to which S-X aircraft will begin to enter service with the troops to replace outdated S-1s from the end of 2011. In accordance with the tactical and technical specifications load capacity C-X there will be 26 tons or up to 110 personnel, and the flight range will be about 6,500 km.

Training Command(UK) is intended for training personnel for the Air Force. It has been operating since 1959, and in 1988, as part of the reorganization of this type, it was reorganized. The command structure includes two fighter and three training wings, an officer candidate school and five aviation technical schools. The total number of permanent personnel of the Criminal Code is about 8 thousand people.

Fighter and training aviation wings are designed to train students and cadets in aircraft piloting techniques. In their organizational structure, these air wings are similar to the two-squadron BAC fighter wing. In addition, in 4 acre there is a demonstration and aerobatic squadron "Blue Impuls" (T-4 aircraft).

The training of pilots of fighter, military transport and search and rescue aviation of the Japanese Air Force is carried out in educational institutions and combat aviation units. It includes three main stages:

Training cadets in piloting techniques and the basics of combat use of combat training aircraft;

Mastering the technique of piloting and combat use of fighters, military transport aircraft and helicopters in service with the Air Force;

Improving the training of flight personnel of aviation units during their service.

The duration of training at a military aviation educational institution from the moment of enrollment until the assignment of the initial officer rank of lieutenant is five years and three months. Air Force educational institutions accept young men aged 18 to 21 with secondary education.

At the preliminary stage, there is an initial selection of candidates for training, carried out by officers of the prefectural recruiting centers. It includes reviewing applications, getting acquainted with the candidates’ personal data and passing a medical commission. Candidates who successfully complete this stage take entrance exams and undergo professional aptitude testing. Applicants who pass the exams with a grade of at least “good” and pass testing become cadets of the Japanese Air Force. The annual intake is about 100 people, of which up to 80 are high school graduates, the rest are graduates civil institutions who expressed a desire to become military pilots.

As part of theoretical training, before starting flight training, cadets study aerodynamics, aircraft technology, documents regulating flight operations, communications and radio equipment, and also acquire and consolidate skills in working with aircraft cockpit equipment during comprehensive training sessions. Duration of training is two years. After this, the cadets are transferred to the first year of initial flight training (on aircraft with piston engines).

The duration of the first stage (on combat training aircraft) is eight months, the program is designed for 368 hours (138 hours of ground training and 120 hours of command and staff training, 70 hours of flight time on T-3 aircraft, as well as 40 hours of training on simulators). The training is organized on the basis of the 11th and 12th training aircraft, which are equipped with T-3 training aircraft (up to 25 units each), simulators and other necessary equipment. The total number of permanent staff (teachers, instructor pilots, engineers, technicians, etc.) of one air wing is 400-450 people, cadets 40-50.

Individual training of pilots is considered the basis for high combat training of flight personnel.

The flight instructors have significant experience in combat and training units. The minimum total flight time of an instructor is 1,500 hours, the average is 3,500 hours. Each of them is assigned no more than two cadets for the training period. Their mastering of piloting techniques is carried out according to the principle “from simple to complex” and begins with practicing take-off, circling flight, landing, and simple aerobatics in the zone. Quite stringent requirements are imposed on cadets' piloting techniques, the need for which is determined by considerations of ensuring flight safety and achieving high professionalism of future pilots. In this regard, the number of cadets expelled due to professional incompetence is quite large (15-20 percent). After completing the first course of initial flight training, cadets are trained in accordance with their desires and demonstrated professional abilities in training programs for fighter and military transport aviation pilots, as well as helicopter pilots.

The fighter pilot training program begins with the second year of initial training (on jet-powered aircraft).

The duration of training is currently 6.5 months. The training program includes ground (321 hours, 15 training topics) and command and staff (173 hours) training, 85 hours of flight time on T-2 jet combat training aircraft (UBS), as well as complex training on the S-11 simulator (15 hours). Training under the second-year program is organized on the basis of the 13th training wing. The total number of permanent personnel of the wing is 350 people, including 40 instructor pilots, whose average flight time on all types of aircraft is 3,750 hours. During training, up to 10 percent. cadets are expelled due to professional incompetence.

The demonstration and aerobatic squadron "Blue Impuls" 4 acre is equipped

by T-4 aircraft

Having completed initial flight training on piston and jet aircraft with a total flight time of 155 hours, cadets proceed to the main course of training, which is conducted on the basis of the 1st Fighter Wing on Japanese-made T-4 aircraft. The program of this training course lasts 6.5 months. It provides for a total flight time of 100 hours for each cadet, ground training (240 hours) and classes in command and staff disciplines (161 hours). Up to 10 percent cadets who have not mastered piloting techniques within the framework installed by the program number of export flights are deducted. Graduates of the basic flight training course are awarded a pilot qualification and awarded the corresponding badges.

The goal of the second stage of flight training for cadets is to master the techniques of piloting and combat use of aircraft in service with the Air Force. In the interests of solving these problems, combat training courses have been organized on T-2 supersonic jet trainers and retraining courses on F-15J and F-4EJ combat aircraft.

The T-2 combat training course is conducted at the 4th Fighter Wing, staffed by instructor pilots with significant experience flying F-4E and F-15 combat aircraft. It is designed for ten months. The program provides for a total cadet flight time of 140 hours. Independent training flights account for approximately 70 percent. total flight time. At the same time, trainees develop stable skills in piloting and combat use of T-2 aircraft. Feature training - participation of cadets, as they gain experience, in joint tactical flight training with pilots of combat units to practice issues of conducting air battles fighters various types. After completing the combat training course on T-2 aircraft, the total flight time of the cadets is 395^00 hours and they are assigned military rank non-commissioned officer. Theoretical and practical retraining is carried out in the 202nd (F-15J aircraft) and 301 (F-4EJ) air defense fighter aviation squadrons, which, along with performing this task, are involved in combat duty. During it, cadets practice the basic elements of piloting techniques and combat use of F-15J and F-4EJ aircraft.

The retraining program for F-15J aircraft is designed to last 17 weeks. It includes theoretical training, training on TF-15 simulators (280 hours) and flights (30 hours). In total, there are 26 pilots in 202 IAE, of which 20 are instructor pilots, each of whom is assigned one cadet for the training period. Retraining for F-4EJ aircraft is carried out at the 301st Air Defense Fighter Squadron for 15 weeks (during this time the cadet's flight time is 30 hours). The theoretical training and simulator training program is designed for 260 training hours.

Training of pilots on military aviation aircraft and helicopters is carried out on the basis of the 403rd air transport wing and the training squadron of the search and rescue aircraft. Most of These pilots are trained by retraining former fighter pilots for military transport aircraft and helicopters, and about half are trained as cadets, who, like future fighter pilots, first study in the theoretical training unit (two years) and pass the first year initial flight training (eight months, on T-3 aircraft), after which they master piloting techniques on the T-4 training aircraft, and then on the B-65 training aircraft. Further, future military transport aviation pilots undergo training on YS-11, S-1 aircraft and S-62 helicopters.

Before being awarded the officer rank of lieutenant, all cadets who have completed retraining and flight practice in units are sent to a four-month command and staff course for flight personnel at the officer candidate school in Nara (Honshu Island). After completing the courses, they are distributed to combat aviation units, where their further training is carried out in accordance with the plans and programs developed by the Japanese Air Force command.

The third stage - improving the training of flight personnel of aviation units during service - is provided for in the process of combat training. Individual training of pilots is considered the basis for high professional and combat training of flight personnel. Based on this, the Japanese Air Force has developed and is implementing plan increasing the annual flight hours of fighter aviation pilots. Flight personnel improve their skills in accordance with special Air Force combat training programs, which provide for the consistent development of elements of combat use independently, as part of a pair, flight, squadron and wing. The programs are being developed by the headquarters of the Japanese Air Force in cooperation with the headquarters of the 5th VA of the US Air Force (AvB Yokota, Honshu Island). The highest form of combat training for flight personnel is flight tactical exercises and training, conducted both independently and jointly with US aviation stationed in the western part of Pacific Ocean.

Every year, the Japanese Air Force hosts a significant number of OBP events on the scale of air wings, aviation directions, important place among which are flight tactical exercises and competitions of the air units of the BAC and the transport air wing. Among the largest are the final exercises of national air force"Soen", the Japanese-American tactical flight exercise "Cope North", as well as joint search and rescue units. In addition, Japanese-American tactical flight training to intercept B-52 strategic bombers in electronic countermeasures conditions and weekly training of fighter aircraft crews in the areas of the Okinawa and Hokkaido islands are systematically organized.

Carrying out scientific research, experiments and tests in the interests of improving aviation equipment and weapons of the Air Force are entrusted to test command. Organizationally, the command structure includes a test wing, an electronic weapons testing group and an aviation medicine research laboratory. The test wing performs the following functions: is engaged in testing and studying the flight, operational and tactical characteristics of aircraft, aviation weapons, electronic and special equipment; develops recommendations for their operation, piloting and combat use; conducts control flights of aircraft arriving from manufacturing plants. Test pilots are also trained at its base. In its activities, the wing is in close contact with the research and technical center.

The Logistics Command is dedicated to solving Air Force logistics problems. It is responsible for receiving and creating inventories material resources, their storage, distribution and maintenance. Organizationally, the command structure includes four supply bases.

In general, the attention paid by the military-political leadership of the country to the development of the national air force indicates important role this high-tech branch of the armed forces is part of Tokyo's plans to ensure the country's combat readiness.

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

Formally, this organization is not a military force and is considered a civilian agency in Japan itself. The Prime Minister of Japan commands the Self-Defense Forces. However, this “non-military organization” with a budget of $59 billion and a staff of almost 250,000 people is equipped with quite modern technology.

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

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

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

After the adoption and start of licensed production of the F-86F aircraft, the Air Self-Defense Forces required two-seat jet trainers (JTS) with characteristics similar to combat fighters. The T-33 straight-wing jet trainer, produced under license by the Kawasaki Corporation (210 aircraft built), based on the first production American jet fighter F-80 Shooting Star, did not fully meet the requirements.

In this regard, the Fuji company developed the T-1 trainer based on the American F-86F Saber fighter. Two crew members were seated in the cockpit in tandem under a common canopy that folded back. The first plane took off in 1958. Due to problems with fine-tuning the Japanese-developed engine, the first version of the T-1 was equipped with imported British Bristol Aero Engines Orpheus engines with a thrust of 17.79 kN.

Japanese training center 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 from 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 the Japanese Ishikawajima-Harima J3-IHI-3 engine with a thrust of 11.77 kN. Thus, the T-1 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 training aircraft for more than 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 take-off weight of up to 5 tons, the aircraft reached speeds of up to 930 km/h. It was armed with one 12.7 mm machine gun and could carry a combat load in the form of NAR or bombs weighing up to 700 kg. In its main characteristics, the Japanese T-1 approximately corresponded to the widespread Soviet training device - UTI MiG-15.

In 1959, the Japanese company Kawasaki acquired a license to produce the Lockheed P-2H Neptune maritime anti-submarine patrol aircraft. Since 1959, mass production began at the plant in the city of Gifu, ending with the production of 48 aircraft. In 1961, Kawasaki began developing its own modification of the Neptune. The aircraft was designated P-2J. Instead of piston engines, it was equipped with two General Electric T64-IHI-10 turboprop engines with a power of 2850 hp each, produced in Japan. The Westinghouse J34 auxiliary turbojet engines were replaced with Ishikawajima-Harima IHI-J3 turbojet engines.

In addition to the installation of turboprop engines, there were other changes: the fuel supply was increased, and new anti-submarine and navigation equipment was installed. In order to reduce drag, the engine nacelles were redesigned. To improve takeoff and landing characteristics on soft ground, the landing gear was redesigned - instead of one large-diameter wheel, the main struts received twin wheels of 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 subsonic jet fighters F-86 by the beginning of the 60s were no longer suitable modern requirements, the command of the Self-Defense Forces began to look for a replacement for them. In those years, the concept became widespread that air combat in the future would be reduced to supersonic interception of strike aircraft and missile duels between fighters.

These ideas were fully consistent with the Lockheed F-104 Starfighter supersonic fighter developed in the United States in the late 50s.

During the development of this aircraft, high speed characteristics were put at the forefront. The Starfighter was subsequently often called “a rocket with a man inside.” US Air Force pilots quickly became disillusioned with this capricious and unsafe aircraft, and they began to offer it to the allies.

In the late 1950s, the Starfighter, despite its high accident rate, became one of the main air force fighters in many countries and was produced in various modifications, including in Japan. It was the F-104J all-weather interceptor. On March 8, 1962, the first Japanese-assembled Starfighter was rolled out of the gates of the Mitsubishi plant in Komaki. In design, it was almost no different from the German F-104G, and the letter “J” only denotes the customer country (J - Japan).

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

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

The passenger turboprop aircraft, designated YS-11, was intended to replace the Douglas DC-3 on domestic routes and could carry up to 60 passengers at a cruising speed of 454 km/h. From 1962 to 1974, 182 aircraft were produced. To this day, 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 retire all variants of the YS-11.

By the mid-1960s, the F-104J began to be regarded as an obsolete aircraft. Therefore, in January 1969, the Japanese Cabinet raised the issue of equipping the country's air force with new interceptor fighters, which were supposed to replace the Starfighters. The American multirole fighter of the third generation F-4E Phantom was chosen as the prototype. But the Japanese, when ordering the F-4EJ variant, stipulated that it be a “pure” interceptor fighter. The Americans did not object, and all equipment for working against ground targets was removed from the F-4EJ, but the air-to-air weapons were strengthened. Everything in this was done in accordance with the Japanese concept of "defense only."

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

A “softening” of Tokyo’s approaches to offensive 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 “Guiding Principles of Japan-US Defense Cooperation.” Before this, there had been no joint actions, not even exercises, between the self-defense forces and American units on Japanese territory. Since then, much has changed, including in the performance characteristics of aircraft, in the Japanese Self-Defense Forces in anticipation of joint offensive actions.

For example, in-flight refueling equipment began to be installed on F-4EJ fighters that were still in production. 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 capabilities. These aircraft were named Kai. Most of the Phantoms that had a large residual life were modernized.

F-4EJ Kai fighters continue to be in service with the Japan Air Self-Defense Force. IN Lately 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, vehicles of this type will be completely written off 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 creating a new generation anti-submarine seaplane. Design was completed in 1966, and the first prototype flew in 1967.

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

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

In January 1973, the first aircraft entered service. The prototype and two pre-production aircraft were followed by a batch of 12 production aircraft, and then eight more aircraft. Six PS-1s were lost during service.

Subsequently Naval forces self-defense refused to use the PS-1 as an anti-submarine aircraft, and all the remaining aircraft in service were focused on search and rescue tasks at sea; anti-submarine equipment from seaplanes was dismantled.

Seaplane US-1A

In 1976, a search and rescue version of the US-1A appeared with higher-power T64-IHI-10J engines of 3490 hp. Orders for the new US-1A were received in 1992-1995, with a total of 16 aircraft ordered by 1997.
Currently, Japanese naval aviation operates two US-1A search and rescue aircraft.

A further development of this seaplane was the US-2. It differs from the US-1A in its glazed cockpit and updated on-board equipment. The aircraft was equipped with new Rolls-Royce AE 2100 turboprop engines with a power of 4500 kW. The design of the wings with integrated fuel tanks was changed. The search and rescue variant also has a new Thales Ocean Master radar in the bow. A total of 14 US-2 aircraft were built, and five aircraft of this type are used in naval aviation.

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

In 1966, Kawasaki, the main contractor of the Nihon Aeroplane Manufacturing Company (NAMC) consortium, began developing a twin-engine jet military transport aircraft (MTC) according to the specifications of the Japan Air Self-Defense Force. The designed aircraft, intended to replace outdated American-made piston transport aircraft, received the designation S-1. The first of the prototypes took off in November 1970, and flight testing was 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. The S-1's avionics allow it to fly in difficult weather conditions at any time of the day.

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

In 1973, an order was received for the first batch of 11 vehicles. The modernized and modified version based on operating experience received the designation S-1A. Its production ended in 1980, with a total of 31 vehicles of all modifications built. The main reason for the cessation of production of the C-1A was pressure from the United States, which saw the Japanese transporter as a competitor to its C-130.

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

In the early 70s it was put into service European countries SEPECAT Jaguar began to arrive, and the Japanese military expressed a desire to have an aircraft of a similar class. Just at the same time, in Japan, the Mitsubishi company was developing the T-2 supersonic training aircraft. It first flew in July 1971, becoming the second jet trainer developed in Japan and the first Japanese supersonic aircraft.

Japanese training center T-2

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

A significant part of the components on this machine were imported, including R.B. engines. 172D.260-50 “Adur” from Rolls-Royce and Turbomeka with a static thrust of 20.95 kN without boost and 31.77 kN with boost each, produced under license by the Ishikawajima company. A total of 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 take-off weight of 12,800 kg, a maximum speed at altitude of 1,700 km/h, and a ferry range with PTB of 2,870 km. The armament consisted of a 20 mm cannon, missiles and bombs on seven hardpoints, weighing up to 2700 kg.

In 1972, the Mitsubishi company, commissioned by the Air Self-Defense Forces, began developing the F-1 combat single-seat fighter-bomber based on the T-2 training facility - 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 aircraft built. A total of 77 F-1 fighter-bombers were delivered to the Air Self-Defense Forces. For comparison: SEPECAT 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 training and training pilots, the T-2 turned out to be very expensive to operate, and its flight characteristics did not meet the requirements for training equipment. The F-1 fighter-bomber, while similar to the Jaguar, was seriously inferior to the latter in combat load and range.

Based on materials:
Encyclopedia of modern military aviation 1945-2002 Harvest, 2005.
http://www.defenseindustrydaily.com
http://www.hasegawausa.com
http://www.airwar.ru

Japanese aviation in World War II. Part one: Aichi, Yokosuka, Kawasaki Andrey Firsov

The origins and pre-war development of Japanese aviation

Back in April 1891, one enterprising Japanese Chihachi Ninomiya successfully launched models with a rubber motor. He later designed a larger model driven by a pusher screw clock mechanism. The model flew successfully. But the Japanese army showed little interest in it, and Ninomiya abandoned his experiments.

On December 19, 1910, Farman and Grande aircraft made their first flights in Japan. Thus began an era in Japan aircraft heavier than air. A year later, one of the first Japanese pilots, Captain Tokigwa, designed an improved version of Farmaya, which was built by the aeronautical unit in Nakano near Tokyo, and which became the first aircraft produced in Japan.

Following the acquisition of several types of foreign aircraft and the production of their improved copies, the first aircraft of original design was built in 1916 - the Yokoso-type flying boat, designed by First Lieutenant Chikuhe Nakajima and Second Lieutenant Kishichi Magoshi.

The big three of the Japanese aviation industry - Mitsubishi, Nakajima and Kawasaki - began operations in the late 1910s. Mitsubishi and Kawasaki were previously heavy industrial enterprises, and Nakajima was backed by the influential Mitsui family.

Over the next fifteen years, these companies produced exclusively foreign-designed aircraft - mainly French, English and German models. At the same time, Japanese specialists underwent training and internships at enterprises and higher engineering schools in the United States. However, by the early 1930s, the Japanese Army and Navy came to the conclusion that it was time for the aviation industry to stand on its own feet. It was decided that in the future only aircraft and engines of our own design would be accepted into service. This, however, did not stop the practice of purchasing foreign aircraft to familiarize themselves with the latest technical innovations. The basis for the development of Japan’s own aviation was the creation of aluminum production facilities in the early 30s, which made it possible to produce 19 thousand tons annually by 1932. "winged metal"

By 1936, this policy had yielded certain results - the Japanese independently designed twin-engine bombers Mitsubishi Ki-21 and SZM1, reconnaissance aircraft Mitsubishi Ki-15, carrier-based bomber Nakajima B51CH1 and carrier-based fighter Mitsubishi A5M1 - all equivalent or even superior to foreign models.

Beginning in 1937, as soon as the “second Sino-Japanese conflict” broke out, the Japanese aviation industry closed itself with a veil of secrecy and sharply increased aircraft production. In 1938, a law was passed requiring the establishment of state control over all aviation companies with a capital of more than three million yen; the government controlled production plans, technology and equipment. The law protected such companies - they were exempt from taxes on profits and capital, and their export obligations were guaranteed.

In March 1941, the aviation industry received another impetus in its development - the imperial fleet and army decided to expand orders to a number of companies. The Japanese government could not provide funds to expand production, but guaranteed loans from private banks. Moreover, the navy and army, which had production equipment at their disposal, rented it out to various aviation companies depending on their own needs. However, army equipment was not suitable for the production of naval products and vice versa.

During the same period, the Army and Navy established standards and procedures for accepting all types of aviation materials. A staff of technicians and inspectors monitored production and compliance with standards. These officers also exercised control over the management of the firms.

If you look at the dynamics of production in the Japanese aircraft industry, you can note that from 1931 to 1936, aircraft production increased three times, and from 1936 to 1941 - four times!

With the outbreak of the Pacific War, these Army and Navy services also participated in production expansion programs. Since the navy and army issued orders independently, the interests of the parties sometimes collided. What was missing was interaction, and, as might be expected, the complexity of production only increased from this.

Already in the second half of 1941, problems with the supply of materials became more complicated. Moreover, the shortage immediately became quite acute, and the issues of distribution of raw materials were constantly becoming more complicated. As a result, the army and navy established their own control over raw materials depending on their spheres of influence. Raw materials were divided into two categories: materials for production and materials for expansion of production. Using a production plan for next year, headquarters distributed raw materials according to the requirements of manufacturers. Orders for components and assemblies (for spare parts and for production) were received by manufacturers directly from headquarters.

Problems with raw materials were complicated by a constant shortage of labor, and neither the navy nor the army was involved in the management and distribution of labor. Manufacturers themselves recruited and trained personnel as best they could. Moreover, with astonishing shortsightedness, the armed forces constantly called up civilian workers in ways completely inconsistent with their qualifications or production needs.

In order to unify the production of military products and expand aircraft production, in November 1943 the Japanese government created the Ministry of Supply, which was in charge of all production issues, including labor reserves and the distribution of raw materials.

To coordinate the work of the aviation industry, the Ministry of Supply has established a certain system for developing a production plan. The General Staff, based on the current military situation, determined the needs for military equipment and sent them to the naval and military ministries, which, after approval, sent them for approval to the ministries, as well as the corresponding naval and army general staffs. Next, the ministries coordinated this program with manufacturers, determining the needs for capacity, materials, human resources and equipment. Manufacturers determined their capabilities and sent a protocol of approval to the ministries of the navy and army. Ministries and general staffs Together they determined a monthly plan for each manufacturer, which they sent to the Ministry of Supply.

Table 2. Aviation production in Japan during the Second World War

	1941	1942	1943	1944	1945
Fighters	1080	2935	7147	13811	5474
Bombers	1461	2433	4189	5100	1934
Scouts	639	967	2070	2147	855
Educational	1489	2171	2871	6147	2523
Others (flying boats, transport, gliders, etc.)	419	355	416	975	280
Total	5088	8861	16693	28180	11066
Engines	12151	16999	28541	46526	12360
Screws	12621	22362	31703	54452	19922

For production purposes, aircraft components and parts were divided into three classes: controlled, distributed by the government, and supplied by the government. “Controlled materials” (bolts, springs, rivets, etc.) were produced under government control, but distributed according to manufacturers' orders. Government-distributed components (radiators, pumps, carburetors, etc.) were produced according to special plans by a number of subsidiaries for delivery to aircraft and aircraft engine manufacturers directly to the latter's assembly lines. Government-supplied components and parts (wheels, weapons, radio equipment, etc. .p.) were ordered directly by the government and delivered as directed by the latter.

By the time the Ministry of Supply was formed, an order was received to stop the construction of new aviation facilities. It was obvious that there was enough capacity, and the main thing was to increase the efficiency of existing production. To strengthen control and management in production, they were represented by numerous inspectors from the Ministry of Trade and Industry and observers from the navy and army, who were at the disposal of the regional centers of the Ministry of Supply.

Contrary to this rather impartial system of production control, the army and navy did their best to maintain their special influence, sending their own observers to aircraft, engine and related industries, and also did everything to maintain their influence in those factories that were already under their control . In terms of the production of weapons, spare parts and materials, the navy and army created their own capacities, without even informing the Ministry of Supply.

Despite the hostility between the navy and the army, as well as the difficult conditions under which the Ministry of Supply operated, the Japanese aviation industry was able to continuously increase aircraft production from 1941 to 1944. In particular, in 1944, production at controlled factories alone increased by 69 percent compared to the previous year. Engine production increased by 63 percent, propellers by 70 percent.

Despite these impressive successes, it was still not enough to counter the enormous power of Japan's opponents. Between 1941 and 1945, the United States produced more aircraft than Germany and Japan combined.

Table 3 Aircraft production in some countries of the warring parties

	1941	1942	1943	1944	Total
Japan	5088	8861	16693	28180	58822
Germany	11766	15556	25527	39807	92656
USA	19433	49445	92196	100752	261826
USSR	15735	25430	34900	40300	116365

Table 4. Average number of people employed in the Japanese airline industry

	1941	1942	1943	1944	1945
Aircraft factories	140081	216179	309655	499344	545578
Engine factories	70468	112871	152960	228014	247058
Screw production	10774	14532	20167	28898	32945
Total	221323	343582	482782	756256	825581

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The aircraft was produced by Kawasaki in 1935-1938. It was an all-metal biplane with a fixed landing gear and an open cockpit. A total of 588 vehicles were produced, incl. Ki-10-I – 300 vehicles and Ki-10-II – 280 vehicles. Performance characteristics of the vehicle: length – 7.2 m; height – 3 m; wingspan – 10 m; wing area - 23 m²; empty weight – 1.4 t, take-off weight – 1.7 t; engine - Kawasaki Ha-9 with 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 heavy night fighter was produced by Kawasaki in 1942-1945. A total of 1.7 thousand vehicles were produced in four production versions: Ki-45 KAIa, Ki-45 KAIb, Ki-45 KAIc and Ki-45 KAId. Vehicle performance characteristics: length – 11 m; height – 3.7 m; wingspan – 15 m; wing area – 32 m²; empty weight – 4 t, take-off weight – 5.5 t; engines - two Mitsubishi Ha-102 with a power of 1,080 hp; 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 No-203 cannon, two 20 mm Ho-5, 7.92 mm Type 98 machine gun; 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-monocoque fuselage structure, pilot armor protection and protected tanks. A total of 3.2 thousand vehicles were produced in two serial modifications: Ki-61-I and Ki-61-II, which differed in equipment and armament. Vehicle performance characteristics: length – 9.2 m; height – 3.7 m; wingspan – 12 m; wing area – 20 m²; empty weight – 2.8 t, take-off weight – 3.8 t; engine - Kawasaki Ha-140 with a power of 1,175 - 1,500 hp; volume of fuel tanks – 550 l; rate of climb – 13.9 – 15.2 m/s; maximum speed - 580 - 610 km/h, cruising speed - 450 km/h; practical range – 1,100 – 1,600 km; practical ceiling – 11,000 m; armament - two 20-mm No-5 cannons, two 12.7-mm Type No-103 machine guns, 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 modifications: Ki-100-Іа and Ki-100-Ib. Vehicle performance characteristics: length – 8.8 m; height – 3.8 m; wingspan – 12 m; wing area – 20 m²; empty weight – 2.5 t, take-off weight – 3.5 t; engine – Mitsubishi Ha 112-II with a power of 1,500 hp, rate of climb – 16.8 m/s; maximum speed – 580 km/h, cruising speed – 400 km/h; practical range – 2,200 km; practical ceiling – 11,000 m; armament - two 20-mm No-5 cannons 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. Vehicle performance characteristics: length – 11.5 m; height – 3.7 m; wingspan - 15.6 m; wing area – 34 m²; empty weight – 5 t, take-off weight – 7.3 t; engines - two Mitsubishi Ha-112 with a power 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 No-401 cannon, two 20-mm No-5 cannons and a 12.7-mm Type No-103 machine gun; bomb load - 500 kg; crew - 2 people.

The N1K-J Shiden, a single-seat all-metal fighter, 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. Performance characteristics of the vehicle: length – 8.9 – 9.4 m; height – 4 m; wingspan – 12 m; wing area – 23.5 m²; empty weight – 2.7 – 2.9 t, take-off weight – 4.3 – 4.9 t; engine – Nakajima NK9H with a power of 1,990 hp; rate of climb – 20.3 m/s; maximum speed – 590 km/h, cruising speed – 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 all-metal interceptor fighter 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). Vehicle performance characteristics: length – 10 m; height – 4 m; wingspan - 10.8 m; wing area - 20 m²; empty weight – 2.5 t, take-off weight – 3.4 t; engine - Mitsubishi MK4R-A with a power of 1,820 hp; rate of climb – 16 m/s; maximum speed – 612 km/h, cruising speed – 350 km/h; practical range – 1,900 km; practical ceiling – 11,700 m; armament - four 20-mm Type 99 cannons; bomb load - 120 kg; crew - 1 person.

An all-metal night twin-engine fighter was produced by Mitsubishi based on the Ki-46 reconnaissance aircraft in 1944-1945. It was a low-wing monoplane with a retractable tail wheel. A total of 613 thousand cars were produced. Vehicle performance characteristics: length – 11 m; height – 3.9 m; wingspan - 14.7 m; wing area – 32 m²; empty weight – 3.8 t, take-off weight – 6.2 t; engines - two Mitsubishi Ha-112 with a power of 1,500 hp; volume of fuel tanks – 1.7 thousand liters; rate of climb – 7.4 m/s; maximum speed – 630 km/h, cruising speed – 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 interceptor fighter was produced by Mitsubishi in 1944 on the basis of the Ki-67 bomber. A total of 22 cars were produced. Vehicle performance characteristics: length – 18 m; height – 5.8 m; wingspan - 22.5 m; wing area – 65.9 m²; empty weight – 7.4 t, take-off weight – 10.8 t; engines - two Mitsubishi Ha-104 with a power of 1900 hp; rate of climb – 8.6 m/s; maximum speed – 550 km/h, cruising speed – 410 km/h; practical range – 2,200 km; practical ceiling – 12,000 m; armament - 75 mm Type 88 cannon, 12.7 mm Type 1 machine gun; 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. Vehicle performance characteristics: 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 weight - 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 speed – 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 Nakajima 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 a fixed landing gear. A total of 3.4 thousand cars were produced. Vehicle performance characteristics: length – 7.5 m; height – 3.3 m; wingspan - 11.4 m; wing area – 18.6 m²; empty weight – 1.2 t, take-off weight – 1.8 t; engine - Nakajima Ha-1 with a power of 650 hp; rate of climb – 15.3 m/s; maximum speed – 470 km/h, cruising speed – 350 km/h; practical range – 1,700 km; practical ceiling – 10,000 m; armament - 12.7 mm Type 1 machine gun and 7.7 mm Type 89 machine gun or two 7.7 mm machine guns; bomb load - 100 kg; crew - 1 person.

Nakajima Ki-43 Hayabusa fighter

The aircraft was produced by Nakajima in 1942-1945. It was an all-metal, single-engine, single-seat, cantilever low-wing aircraft. The rear part 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 its area. A total of 5.9 thousand vehicles were produced in three serial modifications - Ki-43-I/II/III. Vehicle performance characteristics: length – 8.9 m; height – 3.3 m; wingspan - 10.8 m; wing area – 21.4 m²; empty weight – 1.9 t, take-off weight – 2.9 t; engine - Nakajima Ha-115 with a power of 1,130 hp; rate of climb – 19.8 m/s; fuel tank volume – 563 l; maximum speed – 530 km/h, cruising speed – 440 km/h; practical range – 3,200 km; practical ceiling – 11,200 m; armament - two 12.7 mm No-103 machine guns or two 20 mm Ho-5 cannons; 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 wing with all-metal flaps equipped with a hydraulic drive. The pilot's cabin was covered with a teardrop-shaped canopy for all-round visibility. The landing gear is tricycle with two main struts and a tail wheel. During flight, all landing gear wheels were retracted by a hydraulic system and covered with shields. A total of 1.3 thousand aircraft were produced. Vehicle performance characteristics: length – 8.9 m; height – 3 m; wingspan – 9.5 m; wing area – 15 m²; empty weight – 2.1 t, take-off weight – 3 t; engine - Nakajima Ha-109 with a power of 1,520 hp; fuel tank volume – 455 l; rate of climb – 19.5 m/s; maximum speed – 605 km/h, cruising speed – 400 km/h; practical range – 1,700 km; practical ceiling – 11,200 m; armament - four 12.7-mm No-103 machine guns or two 40-mm Ho-301 cannons, 760 rounds of ammunition; bomb load - 100 kg; crew - 1 person.

The 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-Iа/b/с and Ki-84-II. It was a cantilever low-wing monoplane of all-metal construction. It had pilot armor, protected fuel tanks and retractable landing gear. Vehicle performance characteristics: length – 9.9 m; height – 3.4 m; wingspan – 11.2 m; wing area – 21 m²; empty weight – 2.7 t, take-off weight – 4.1 t; engine - Nakajima Na-45 with a power of 1,825 - 2,028 hp; fuel tank volume – 737 l; rate of climb – 19.3 m/s; maximum speed - 630 - 690 km/h, cruising speed - 450 km/h; practical range – 1,700 km; practical ceiling – 11,500 m; armament - two 20-mm No-5 cannon, two 12.7-mm Type No-103 machine guns or four 20-mm No-5; bomb load - 500 kg; crew - 1 person.