Category Archives: Fighter

Fighter

Kawasaki Ki-96 (A+V Models, Resin)

TYPE: Twin engine heavy fighter

ACCOMMODATION: Pilot only

POWER PLANT: Two Mitsubishi Ha-12-11 radial engine, rated at 1,500 hp

PERFORMANCE: 391 mph at 31,170 ft

COMMENT: The great success of the Kawasaki Ki-45-KAI “Toryu” (“Dragon Slayer”, Allied code “Nick”) encouraged the Kawasaki Company to initiate work on a refined, more powerful derivative of the Ki-45. Compared with its forerunner an aerodynamically improved fuselage, a larger square-tipped vertical tail surface, and more powerful engines were provided. In 1943 work on the Ki-96 gained tempo and in September that year the first prototype was completed. In the meantime it became obvious that a second crew member was superfluous in a high-performance twin-engined fighter. So the second cockpit of the first prototype was faired over and the two other prototypes under construction were finished as single-seater. Flight test were most satisfactory, the Ki-96 combining good handling characteristics with performance exceeding design estimates. However, the Army’s interest in the potential of single-seat twin-engined fighters was to prove short-lived and consequently the Ki-96 had only a brief live as an aerodynamically prototype for the two-seat Kawasaki Ki-102 which supplanted it (Ref.: 1, 5).

Kawasaki Ki-78 (Planet, Resin)

TYPE: High-speed research aircraft

ACCOMMODATION: Pilot only

POWER PLANT: One Daimler-Benz DB 601A liquid-cooled piston engine, rated at 1,155 hp with Water/Methanol injection                  

PERFORMANCE: 435 mph at 11,500 ft

COMMENT: The Ki-78, designed at the Aeronautical Research Institute and built at Kawasaki Kokuki Kogyo K.K. to investigate flying behaviour at very high speed, featured a streamlined minimum cross-section fuselage fitted with a licence-built Daimler-Benz DB 601A engine. For short duration power boost methanol/water injection was used, and cooling was improved by a 60 hp turbine driven cooling fan for the radiators. By the outbreak of the war, the whole project was taken over by the Imperial Japanese Army who gave it the military type designation Ki-78. Kawasaki received the order to build two prototypes of the Ki-78, construction of which was started in September 1941. The first prototype was completed more than a year later and was flown for the first time on 26 December 1942. A feasibility study to improve the KI-78 flight performance showed that extensive airframe modifications were needed and consequently the project was officially terminated after the 32nd flight on 11 January 1944; the second Ki-78 was never completed (Ref.: 23).

Kawasaki Ki-60 (Airmodel, Resin)

TYPE: Interceptor fighter

ACCOMODATION: Pilot only

POWER PLANT: : One Daimler-Benz DB 601 liquid-cooled inverted V-12 engine, rated at 1,175 hp

PERFORMANCE: 348 mph at 14,800 ft

COMMENT: The Kawasaki Ki-60 was an experimental fighter that used a license-built German Daimler-Benz (Kawasaki) DB 601 liquid-cooled engine. This was at that time an unusual choice because the majority of Japanese aircraft used air-cooled radial engines. The Ki-60 was designed by Kawasaki Aircraft Industries in response to a 1939 Imperial Japanese Army Aviation Bureau requirement for a heavily armed specialised interceptor fighter to be powered by the liquid-cooled Daimler-Benz DB 601 inverted V12 engine, which had been selected for license production by Kawasaki as the Ha-40. A requirement was issued at the same time for a lighter, less heavily armed, general-purpose fighter which was to be designed almost in parallel with the Ki-60; this became the Kawasaki Ki-61 Hien. Priority was to be given to the Ki-60, design of which started in February 1940. The first prototype of the Ki-60 emerged in March 1941 as a compact monoplane with a relatively deep fuselage and tapered wings with rounded tips built around a system of three spars. The pilot’s seat was mounted high over the rear spar, giving the fuselage a distinctive “humped” profile; the hood featured a framed, rear sliding canopy and an elongated rear transparent section. The main coolant radiator was housed in a long ventral bath under the wing center-section and central fuselage, while the oil cooler was mounted under the engine with a long air intake. The prototype was powered by an imported Daimler-Benz DB 601A as production of the Ha-40 had not yet started. Although a top speed of 370 mph had been projected the Ki-60 was only able to achieve 341 mph. By this time the Nakajima Ki-44 Hajabusa, which had also been designed as a dedicated interceptor, was beginning to show some promise and the Koku Hombu selected this in fulfilment of its requirements. From early 1941 the full attention was focused on the Kawasaki Ki-61 Hien, but the Ki-60 became important in that the Ki-61 design was able to be improved using the lessons learned from the poor characteristics of the Ki-60. Plans for production were cancelled in late 1941 after three airplanes had been built. (Ref.: 23)

Nakajima Ki-44-II-Hei Shoki (Devil- Queller, Toyo), 70th Sentai (Hasegawa)

TYPE: Interceptor fighter

ACCOMMODATION: Pilot only

POWER PLANT: One Nakajima Ha-109 radial engine, rated at 1,520 hp

PERFORMANCE: 367 mph at 17,060 ft

COMMENT: The Ki-44-IIc variant of the Nakajima Shoki aircraft was armed with wing-mounted 20 mm Ho-3 cannon that proved particular effective against the B-29’s attacking Japan. But in December 1944, Shoki production terminated as the aircraft was replaced on Nakajima’s assembly-lines by the Nakajima Ki-84 Hayate and, when the war ended, only three Sentais were still equipped with them. In total 1, 225 Ki-44’s were built (Ref.: 1, 6)

Tachikawa Ki-106 (RS Models)

TYPE: Interceptor fighter

ACCOMMODATION: Pilot only

POWER PLANT: One Nakajima Ha-45-21 radial engine, rated at 1,990 hp

PERFORMANCE: 385 mph at 21.325 ft

COMMENT: Although the Nakajima Ki-84 Hayate was one of the most successful Japanese aircraft a modified version seemed to be necessary due to the increasingly critical light alloy supply situation as the war progressed. In late 1943 Tachikawa Hikoki K.K. were entrusted by the Ministry of Munitions with the task of designing an all-wood version of the Ki-84. Work on three airframes, designated Ki-106, began in autumn 1944, but various factors delayed the programme and the first of these prototypes was not to be completed and flown until July 1945. The Ki-106 was heavier than the standard Ki-84 what exerted an adverse effect on maneuverability and climb rate, but maximum level speed was virtually unchanged. The end of the war brought the Ki-106 project to a halt. (Ref.: 1., 6.)

Nakajima Ki-44-IIc-Otsu Shoki (Devil-Queller, Toyo), 87th Sentai, 2nd Chutai (Hasegawa)

TYPE: Interceptor fighter

ACCOMMODATION: Pilot only

POWER PLANT: One Nakajima Ha-109 radial engine, rated at 1,520 hp

PERFORMANCE: 367 mph at 17,060 ft

COMMENT: When China-based B-29s of the US XX Bomber Command, soon joined by Mariana-based Superfortresses of the XXI Bomber Command, began their bombing raids against Japan homeland, the Japanese Army had only one type of interceptor fighter on strength: The Nakjima Ki-44-IIb Shoki, (Devil-Queller) known as TOYO to Allied personel. The first prototype was completed and flown in August 1940 and production of the Ki-44-I started in in January 1942. As war progressed several variants were produced, so as Ki.44-II and Ki-44-III, all with several subtypes and more than nine Sentais and several Fighter Training Schools were equipped with the Ki-44. In late 1944, Shoki production terminated as the aircraft was replaced by the Nakajima Ki-84 Hayate (Ref.: 1).

Kawasaki Ki-119 (Unicraft, Resin)

TYPE: Suicide aircraft, Light bomber, Dive bomber and Escort fighter. Project.

ACCOMMODATION: Pilot only

POWER PLANT: One Mitsubishi Ha-104 radial engine, rated at 1,900 hp

PERFORMANCE: 360 mph at 19,685 ft

COMMENT: In early 1945 the Japanese Army Air Force instructed Kawasaki to proceed immediately with the design of a single-seat light bomber aircraft to supplement the suicide forces in the defense of the homeland. The aircraft had to be easy to manufacture, to maintain and to fly, had a good performance and load-carrying capability. Due to shortage of engine manufacturing facilities, a single-seat and single-engine configuration became attractive. In less than three months the basic design of the aircraft was completed and a mock-up was readied for inspection. The initial plans for the first flight in September 1945 could not be realized due to the collapse of Japan (Ref. 1).

Rikugun Ki-93-Ia (A+V Models, Resin)

TYPE: Twin-engined heavy fighter and ground attack aircraft

ACCOMMODATION: Crew of two

POWE PLANT: Two Mitsubishi Ha-214 radials, rated at 2,400 hp each

PERFORMANCE: 388 mph at 27,230 ft

COMMENT: The Rikugun Ki-93 was the last heavy fighter and ground-attack aircraft built in Japan during WW II and was the only design of the Rikugun Kogugijutsu Kenkyujo (Army Aerotechnical Research Institute) to be flown. Powered by two 2,400 hp Mitsubishi Ha-214 air-cooled radials driving six-blade propellers, the aircraft was designed specially to carry large caliber cannon in its under-fuselage gondola. Thus the Ki-93 was designed to perform as a high-altitude heavy bomber destroyer as well as a low-altitude anti-shipping aircraft. In its bomber destroyer form (Ki-93-Ia ) the aircraft carried offensive armament comprising one 57 mm Ho-401 cannon and two 20 mm Ho-5 cannon, while for the anti-shipping missions its offensive armament  comprised one 75 mm Type 88 cannon and two 250 kg bombs (Ki-93-Ib).
Production of the Ki-93 was entrusted to the Dai-Ichi Rikugun Kokusho (First Army Air Arsenal) at Tachikawa and the first prototype was completed and flown in April 1945. A second prototype, the Ki-93-Ib in ground attack configuration, was completed but not flown before the end of the hostilities. (Ref.: 1)

Nakajima Ki-84-I-Ko Hayate, 1st Chutai, 102nd Hiko Sentai (Hasegawa)

TYPE: Fighter, Fighterbomber

ACCOMMODATION: Pilot only

POWER PLANT: Nakajima Ha-45 engine, rated at 1,990hp

PERFORMANCE: 392 mph at 20,080 ft

COMMENT: In June 1943 some of the first Nakajima Ki-84-Ia  Hayate of a service trials batch of 83 machines were handed over to the Tachikawa Army Air Arsenal for service tests. During flight trials the Ki-84 reached a top speed of 388 mph, climbed to 16,405 ft in 6 min 26 sec and reached a service ceiling of 40,680 ft, thus demonstrating the best performance of any Japanese aircraft suitable for immediate production. A second pre-production batch of 42 Ki-84s was built in April 1944 and in the following months more and more aircraft were delivered to several Sentai. In combat it became obvious that the Ki-84 was a formidable foe , comparing favourably with the best Allied fighters. (Ref.: 1)

Nakajima Ki-84-Ia Hayate, Chutai 29th Hiko Sentai (Hasegawa)

TYPE: Fighter, Fighterbomber

ACCOMMODATION: Pilot only

POWER PLANT: One Nakajima Ha-45 engine, rated at 1,999 hp

PERFORMANCE: 392 mph at 20,080 ft

COMMENT: Undoubtedly the best Japanese fighter aircraft to see large-scale operation during the last years of war in the Pacific Area, was well protected, well armed, fast and manoeuvrable. The Ki-43 Hayabusas were just starting to fire their guns in anger when Nakajima was instructed to design their replacement. The specification called for an all-purpose, long-range fighter with high speed and capable of operating at combat rating for 1.5 hours. Design work was initiated in early 1942 and in March 1943 the first prototype was completed. Flight test began in April 1043 and after success under operational conditions the mass production of the aircraft war started as Army Type 4 Fighter Model 1A Hayate, or Ki-84-Ia. A total of 3,514 Ki-84s and derivatives were built, of which were 3,288 Ki-84-I and Nakajima Ki-84-II production aircraft as well as 3 Tachikawa Ki-106 prototypes, a wooden version of the Ki-84 Hayate. (Ref.: 1)