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Ki-10

Ki-10
  • Fighter
  • First flight: 1935
  • Kawasaki

At the beginning of the 30s of the last century, the aviation of the Imperial Japanese Army consisted mainly of two types of fighters: Nakajima "Army Type 91" and Kawasaki "Army Type 92". The first of these was a monoplane with a parasol wing, and the second was a classic biplane. For their time, these were generally quite successful machines, but in terms of speed they were noticeably inferior to a number of more modern foreign fighters, in particular the English Hawker "Fyori" and the Hcherikan Boeing P-26A. To reduce the speed gap, in 1933, Kawasaki specialists designed a new aircraft, the Ki-5. It was a Fighter monoplane with a "reverse gull" wing and high aerodynamic characteristics, but the military rejected it because, in their opinion, insufficient maneuverability. However, Japanese aviation still needed fast machines, and in September 1934, shortly after the cessation of work on the Ki-5, Kawasaki was instructed to design a Biplane Fighter, and Nakajima was given an order to create a monoplane fighter. The first project was assigned the army designation Ki-10, the second - Ki-11.

At Kawasaki, the development of the new aircraft was led by Takeo Doi. In March 1935, the first prototype of the Ki-10. which is equipped with 850-horsepower 12-cylinder liquid-cooled V-engine Kawasaki Na-9-IIa half-plane with ailerons only on the upper wing, took off. A month later, the second prototype was flown. During the tests, it turned out that the new aircraft surpasses its predecessor Ki-5 in all key indicators, but is still inferior in speed to its competitor, the Nakajima Ki-11 monoplane fighter. In order not to miss out on a lucrative contract, Kawasaki specialists made a number of changes to the design of the third and fourth prototypes: a three-blade metal propeller was installed on the third machine (instead of a two-blade wooden fixed-pitch propeller) and a flush riveting was used, and on the fourth, the transverse V of the wing was increased - for stability improvements. And although the modified Ki-10s were still inferior in speed to the Ki-11s, this difference was compensated by much higher maneuverability, to which the military traditionally attached the greatest importance. As a result, the Fighter "Kawasaki" was launched into the series, which received the designation "Army Fighter Type 95 Model 1" (Ki-10-I). Production aircraft were identical to the third prototype. In total, from December 1935 to October 1937, 300 such aircraft were delivered to the troops.

In June 1937, the Ki-10-I was replaced by an improved version of the Ki-10-II. which differed in a wing of a larger area and scope, as well as a longer fuselage. In addition, machines of this modification showed better stability. Ki-10-II aircraft were produced until December 1938, during which time 280 fighters were built.

In addition to two serial modifications, several experimental variants were also developed. The first of them - Ki-10-I KAI (KAI - from the Japanese Kaizo - modified, special) - was created as a result of refinement of the standard Ki-10-L. The fuselage of the experimental aircraft was distinguished by higher aerodynamic characteristics, the radiator was moved back. The landing gear became cantilever, the wheels were equipped with fairings, which made it possible to increase the maximum speed from 400 to 420 km / h. Later, two copies of the Ki-10-II KAI were built, which differed from the Ki-10-I KAI only in a new engine - a forced Ha 9-IIb, which developed 950 hp at an altitude of 3800 m. The speed of the fighter increased to 445 km / h and almost equaled the speed of the new Nakajima Ki-27 fighter, however, the Ki-10-II KAI did not go into mass production - the time for biplanes had already passed.

Ki-10-I and Ki-10-II aircraft, the most advanced biplane fighters in Japanese aviation, actively participated in the combat operations of the Sino-Japanese war and in the conflict at Khalkhin Gol. By the beginning of the Pacific War, the Ki-10 was obsolete and used mainly as a trainer, although the Allies, who assigned this Japanese fighter the code name "Perry", believed that the aircraft was still in service with combat units.

Design. Kawasaki Ha-9-IIb 12-cylinder liquid-cooled V-engine with 850 hp.

The Ki-10's wing construction is fabric-covered metal. The span of the upper wing is much larger than the span of the lower. Only the upper wing was equipped with ailerons. The lower wing, in contrast to the upper wing, was characterized by a positive transverse angle V.

The landing gear of the aircraft was made non-retractable. Sometimes, to reduce aerodynamic drag, the wheels were covered with massive fairings.

The fuselage of the Ki-10 had a design typical for many aircraft of those years and was a welded frame with a mixed metal-cloth covering. The cockpit, by tradition, was made open.

Kawasaki Ki-10-II
Crew 1
Dimensions
Wing span, m 10.02
Wing area, m² 23.00
Length, m 7.55
Height, m 3.00
Powerplant
1 × PE Kawasaki Hа-9-IIb
Power, hp[ 1 × 850
Weights, kg
Empty weight 1,360
Loaded weight 1740
Performance
Maximum speed, km/h 400
Maximum rate of climb, m/min 1,000
Service range, km 1,100
Service ceiling, m 11,500
Armament
Two 7.7-mm synchronous machine guns "type 89"
Photo Description
Ki-10

Drawing Ki-10


Ki-11

Ki-11
  • Fighter
  • First flight: 1934
  • Nakajima

At Nakajima, Yasushi Koyama was appointed to lead the development work, and Shinroku Inoue was the chief designer of the project. The new aircraft (trade designation PA) featured a stocky fuselage and swept wings with rounded tips, giving it an elliptical planform. Although Nakajima's previous low wing had a cantilever wing, the thinner profile for higher speeds could only be applied to a wing reinforced with external braces. Therefore, the designers of the campaign went for just such a variant of the wing of the new fighter. The fixed main landing gear was equipped with wide-chord fairings.

Between April and December 1935, four prototypes were built, each with some differences. The third prototype was fitted with a three-bladed propeller, while the fourth was equipped with a two-bladed propeller and a cockpit canopy. Each of the prototypes had differences in the undercarriage fairings and vertical tail, as well as minor changes based on test results.

Joint flight tests of the Ki-10 and Ki-11 took place in mid-1935 at the Army Aircraft Research Institute at Tachikawa and were conducted by its team of test pilots. The ratings of aircraft performance were mainly based on the favorite method of Japanese aviation - maneuverable horizontal battles, which gave the Kawasaki Ki-10 polutoraplan an advantage over the Nakajima Ki-11 monoplane. The latter, in this case, would be more suitable for hit-and-run tactics, the advantages of which were discovered a little later. On the basis of these differences, the Ki-10 won the competition, which was adopted by the Imperial Army and became the "type 95 fighter", while in September 1935 the Ki-11 was rejected. However, reports indicated that the Ki-11's Kotobuki radial engine was more reliable than the Ki-10's Ha-9 II water-cooled inline engine, which was an evolution of the BMW-VI line version. Despite these results, the Ki-11 became the basis for the development of the next generation of Japanese fighters, one of which was the Nakajima Ki-27, which received from the Allies during the Pacific War codename Nate.

Efforts were made by Nakajima to produce the Ki-11 as an export fighter for Southeast Asia, but no potential customers showed any interest in it, and so production was discontinued after four prototypes were built. The first and third prototypes were used by Nakajima for research on new fighter projects, and the fourth was sold to the Asahi Shimbun (朝日新聞 - Morning Sun Newspaper) as a high-speed aircraft (civil registration number J-BBHA) under the designation AN-1.

In the service of the Asahi Shimbun newspaper, this one and only AN-1 achieved significant success. On December 31, 1935, an AN-1 aircraft piloted by Mosaburo Niino set a speed record by flying from Tokyo to Osaka in 1 hour and 25 minutes. This record was surpassed by the same aircraft when Masaaki Iinuma flew this route. In June 1936, during a solar eclipse best seen on the island of Hokkaido, a piloted Iinuma AN-1 delivered undeveloped films to the newspaper's Tokyo office, outpacing all other newspaper competitors. This flight was performed at an average speed of 398 km/h. Until the advent of the Mitsubishi Karigane, which was used by the Asahi Shimbun newspaper in March 1937 as an ultra-long-range Kamikaze aircraft, the Nakajima AN-1 remained the fastest Japanese machine. In preparation for the European goodwill flight, Iinuma used the AN-1 to improve its flying skills ahead of the historic flight. The famous French pilot Marcel Doret took off in an AN-1 from Haneda Airport in September 1937, demonstrating his aerobatics skills on this modern aircraft.

Nakajima Ki-11
Crew 1
Dimensions
Wing span, m 10.80
Площадь крыла, м² 18.00
Length, m 7.45
Height, m 3.37
Powerplant
1 × PE Nakajima Kotobuki 3
Power, hp 1 × 710
Weights, kg
Empty weight 1,269
Loaded weight 1,700
Performance
Maximum speed, km/h 420
Cruise speed, km/h 367
Maximum rate of climb, m/min 778
Service range, km 1,100
Service ceiling, m 10,000
Armament
Two 7.7-mm synchronous machine guns "type 89"
Photo Description
Ki-11

Drawing Ki-11

AN-1

Nakajima AN-1

Ki-12

Ki-12
  • Fighter
  • First flight: 1936
  • Nakajima

Despite the failure of the Ki-11, Nakajima continued her research into fast fighters, beginning the design of a new machine with technical assistance from Dewoitine. Roger Robert and Jean Beziaud led the project from the French side, and Shigenobu Mori from the Japanese side. The Dewoitine D.510J fighter was taken as a model, while the project was based on an experienced Ki-11 fighter: leaving the rear fuselage, the design team replaced the Nakajima Kotobuki 3 radial engine with a French Hispano-Suiza 12Xcrs water-cooled engine with a capacity of 610 hp. With..

Nakajima wanted to squeeze the maximum performance out of the aircraft, and therefore its design was distinguished by the use of the latest achievements in aircraft construction, many of which were used for the first time on Japanese fighters. The Ki-12 used retractable hydraulic undercarriages, a slotted wing and cannon armament: a 20 mm cannon was installed on the fighter, firing through the camber of the propeller. On trials in October 1936, the aircraft showed excellent flight performance.

However, the leadership of the army aviation from the very beginning was critical of the f. Nakajima: The victorious supporters of the "maneuverable" fighter considered the Ki-12 to be insufficiently stable, poorly maneuverable (by Japanese standards), expensive and complicated. In addition, in the experience of Kawasaki's problems with the licensed release of the BMW-VI, there were doubts about the ability of the Japanese industry to establish serial production of the Hispano-Suiza 12Xcrs.

All this led to the refusal of the military to accept the Ki-12 into service. As a result, Nakajima also came to the conclusion about the dangers of running ahead of the locomotive: the company began work on a more "simple" project "type P.E." with fixed landing gear and air-cooled engine. The development of the "RE type" project led to the appearance of the Ki-27 fighter, which was put into service.

Nakajima Ki-12
Crew 1
Dimensions
Wing span, m 11.00
Wing area, m² 17,00
Length, m 8.30
Height, m 3.45
Powerplant
1 × PE Hispano-Suiza 12Xcrs, power hp 1 × 610
Weights, kg
Empty weight 1,400
Loaded weight 1,900
Performance
Maximum speed, km/h 480
Cruise speed, km/h 425
Service range, km 800
Service ceiling, m 10,500
Armament
20-mm cannon Hispano-Suiza HS.404 1
7.7-mm synchronous machine gun "type 89" 2

Bibliography

  • Japanese aircraft of World War II. /Oleg Doroshkevich/
  • Japanese aviation. /A. Firsov/
  • Fighter "Kawasaki" Ki-10 / Planes of the World. Elena Astakhova./
  • Experienced fighter Nakajima Ki-11 /Alternative History/
  • The one who is unlucky. Fighter Nakajima Ki-12 /Alternative History/
  • Encyclopedia of military equipment /Aerospace Publishing/