In December 1939 
         Nakajima was instructed by the Imperial Japanese Army to initiate 
         development of a more advanced fighter to supersede the company's own 
         Ki-27, the first of three prototypes making its maiden flight during 
         January 1939. A cantilever low-wing monoplane, this Nakajima Ki-43 had 
         retractable tailwheel landing gear, seated its pilot in an enclosed 
         cockpit and was powered by Nakajima's new supercharged Ha-25 Sakae 
         radial engine with a take off rating of 975 hp (727 kw). Service 
         testing of the prototypes showed that the type met the specification, 
         but manoeuvrability was so poor that, at one time, it seemed the new 
         fighter was unlikely to be accepted by the army. However, 10 
         pre-production aircraft were ordered and in attempts to improved 
         manoeuvrability, modifications were introduced. These included 
         increased wing area, weight reduction and finally, the incorporation of 
         manoeuvrability or so-called combat flaps. This proved to be the answer 
         to the problem, to the extent that the type was ordered into production 
         as the Army Type 1 Fighter Model 1A Hayabusa (Perigrine Falcon), 
         company designation Ki-43-1a.
         
         
         Nakajima Ki-43-Ic of HQ Chutai, 64th Sentai, Chiengmai, northern 
         Thailand in March 1942
         This version was armed 
         with two 7.7 mm (0.303 in) machine guns and carried two 33 lbs (15 kg) 
         bombs on external racks, but two sub-variants differed in armaments, 
         the Ki-43-1b having one 7.7 mm (0.303 in) and one 12.7 mm (0.50 in) and 
         the Ki-43-1c two 2.7 mm (0.50 in) machine guns. Production started 
         March 1941 and when the K-43 began to reach operational units it proved 
         to be by far the most manoeuvrable fighter in the army's inventory, 
         enjoying considerable success in the early stages of the Pacific war. 
         With the advent of more effective allied fighters, however, the Ki-43's 
         shortcomings became apparent, leading first to the construction of five 
         Ki-43-II prototypes for evaluation. These introduced the more powerful 
         Nakajima Ha-115 engine, some armour protection for the pilot, and an 
         early form of self-sealing fuel tanks.
         
         
         Satisfactory testing 
         brought construction of the initial Ki-43-IIa production version which 
         had reduced wing span, a modified canopy, machine gun armament as for 
         the Ki-43-Ic, and two underwing racks each able to carry a 551 lbs (250 
         kg) bomb. Late series aircraft, designated Ki-43-IIb (also known as the 
         Ki-43-II Otsu), were generally similar but for some equipment changes, 
         and the final production Ki-II-KAI incorporated the progressive 
         modifications introduced on the Ki-43-IIa and Ki-43-IIb aircraft. 
         Further development followed with the construction of 10 Ki-43-IIIa 
         prototypes, which which were similar to the Ki-43-II KAI except for 
         introducing the 1,150 hp (858 kw) Nakajima Ha-115-II to give improved 
         performance at rated altitude, and two Ki-43-IIIb interceptor 
         prototypes with the 1,300 hp (969 kw) Mitsubishi Ha-112 engine and 
         forward firing machine armament of two 20 mm cannon, but neither of 
         these versions entered production before the Pacific war ended.
         Allocated the Allied 
         codename 'Oscar', the Hayabusa remained in service from the beginning 
         to the end of the war, taking active part in operations for the defence 
         of Tokyo and by use in a Kamikaze role. Production had totalled 
         5,919 by wars end, with (3,239) built by Nakajima, (2,631) built by 
         Tachikawa and 49 aircraft built by the Army Air Arsenal at Tachikawa.  
         (Army Type 1 Fighter 
         Model 1A Hayabusa "Perigrine Falcon" - Nakajima Ki-43-IIb or Ki-43-II 
         Otsu)
         Allied Codename: 
         Oscar
         Type: Single 
         Seat Fighter & Fighter Bomber
         Powerplant: One 
         1,150 hp (858 kw) Nakajima Ha-115 14-cylinder radial piston engine.
         Performance: 
         Maximum speed 329 mph (530 km/h) at 13,125 ft (400 m); cruising speed 
         273 mph (440 km/h); service ceiling 36,745 ft (11200 m).
         Range: 1,988 
         miles (3200 km) with external fuel stores.
         Weight: Empty 
         4,211 lbs (1910 kg) with a maximum take-off weight of 5,710 lbs (2590 
         kg).
         Dimensions: Span 
         35 ft 6 3/4 in (10.84 m); length 29 ft 3 1/4 in (8.92 m); height 10 ft 
         8 3/4 in (3.27 m); wing area 230.36 sq ft 
         (21.40 sq m).
         Armament: Two 
         12.7 mm (0.50 in) forward firing machine guns, plus two bombs up to 551 
         lbs (250 kg) in weight on underwing racks.
         Variants: Ki-43 
         (prototype), Ki-43-1a (Army type I Fighter Model 1A Hayabusa production 
         aircraft) , Ki-43-1b, Ki-43-1c, Ki-43-II (five prototypes for 
         evaluation), Ki-43-11a (production aircraft), Ki-43-11b, Ki-43-11 KAI, 
         Ki-43-111a (prototype with a more powerful engine), Ki-43-111b 
         (proposed interceptor with only cannon but it never entered service).
         Operators: 
         Japanese Army, Thailand.