Very soon after the 
         design of the Ki-43 Hayabusa had been started by Nakajima, the company 
         received instructions from the Imperial Japanese Army to initiate the 
         design of a new interceptor fighter. In this case however, 
         manoeuvrability was required to give precedence to overall speed and 
         rate of climb, and the company's design team selected the 1,250 hp (932 
         kw) Nakajima Ha-141 as the powerplant for this new project. Of similar 
         configuration to the Ki-43, the new Nakajima Ki-44 prototypes also 
         incorporated the manoeuvring flaps that had been introduced on that 
         aircraft, and carried an armament of two 7.7 mm (0.303 in) and two 12.7 
         mm (0.50 in) machine guns. First flown on August 1940, the Ki-44 was 
         involved in a series of comparative trials against Kawasaki's Ki-60 
         prototype, based on the use of the Daimler-Benz DB 601 engine, and an 
         imported Messerschmitt Bf 109E. The result of the evaluation and 
         extensive service trials, showed the Ki-44 to be good enough to enter 
         production, and it was ordered under the designation Army Type 2 Single 
         seat Fighter Model 1A Shoki (demon), company designation Ki-44-Ia, 
         which carried the same armament as the prototypes. A total of only 40 
         Ki-44-I aircraft was produced, including small numbers of the Ki-44-Ib 
         armed with four 12.7 mm (0.50 in) machine guns, and the similar 
         Ki-44-Ic with some minor refinements. 
         
           
         Nakajima Ki-44-IIb of the 23rd Sentai for home island defence in 1944  
         When introduced into 
         service the high landing speeds and limited manoeuvrability of the 
         Shoki made it unpopular with pilots, and very soon the Ki-44-II with a 
         more powerful Nakajima Ha-109 engine was put into production. Only 
         small numbers of the Ki-44-IIa similarly armed to the Ki-44-Ia, were 
         built, the variant being followed by the major production Ki-44-IIb 
         which apart from the different engine was identical to the Ki-44-Ic. 
         The Ki-44-IIc introduced much heavier armament, comprising of four 20 
         mm cannon or alternatively two 12.7 mm (0.50 in) machine guns and two 
         40 mm cannon, and these proved to be very effective when deployed 
         against Allied heavy bombers attacking Japan. However the increased 
         power had done nothing to eliminate the reasons for its unpopularity 
         with the pilots, and in fact, the higher wing loading of this version 
         meant that it had some violent reactions to high speed manoeuvres; 
         however, it later regained their respect because of its capability as 
         an interceptor. 
         
           
         Nakajima Ki-44-IIb of the Shinten (air superiority) unit of the 47th 
         Sentai, Narimasu, Tokyo, summer 1944
         Final production 
         version was the Ki-44-III with a 2,000 hp (1491 kw) Nakajima Ha-145 
         radial engine, an increase in wing area and enlarged vertical tail 
         surfaces, but comparatively few were built before production ended in 
         late 1944. They included the Ki-44-IIIa and the similar Ki-44-IIIb, 
         armed with four 20 mm cannon, and two 20 mm and two 37 mm cannon 
         respectively. 
         Nakajima had built a 
         total of 1,225 Ki-44's of all versions, including prototypes, and these 
         were allocated the Allied codename 'Tojo'. They were deployed primarily 
         in Japan, but were used also to protect vital targets, as in Sumatra 
         where they defended the oil fields at Palembang.  
         (Army Type 2 Single 
         Seat Fighter Model 1A Shoki "Demon" - Nakajima Ki-44-IIb) 
         Allied Codename: 
         Tojo 
         Type: Single 
         Seat Fighter Interceptor 
         Powerplant: One 
         1,520 hp (1133 kw) Nakajima Ha-109 (Type 2) 14-cylinder radial piston 
         engine. 
         Performance: 
         Maximum speed 376 mph (605 km/h) at 17,060 ft (5200 m); cruising speed 
         249 mph (400 km/h); service ceiling 36,745 ft (11200 m). 
         Range: 1,056 
         miles (1700 km) with internal fuel stores. 
         Weight: Empty 
         4,641 lbs (2105 kg) with a maximum take-off weight of 6,598 lbs (2993 
         kg). 
         Dimensions: Span 
         31 ft 0 in (9.45 m); length 28 ft 10 in (8.79 m); height 10 ft 8 in 
         (3.25 m); wing area 161.46 sq ft (15.00 sq m). 
         Armament: Two 
         12.7 mm (0.50 in) Type I (Ho-103) machine-guns in the upper decking 
         fuselage and two 12.7 mm (0.50 in) Type I (Ho-103) machine-guns mounted 
         in the wings. 
         Variants: Ki-44 
         (prototype SN 4401-4403), Ki-44-I(a) Army Type 2, Ki-44-Ib, Ki-44-Ic, 
         Ki-44-IIa (Nakajima Ha-109 Army Type 2 radial engine rated at 1,450 
         hp), Ki-44-IIb, Ki-44-IIc, Ki-44-IIIa, Ki-44-IIIb (Two 20 mm Ho-5 
         cannons and two 37 mm Ho-203 cannon). 
         Operators: 
         Japanese Army.  |