|Manufacturer||Nakajima Aircraft Company|
|First flight||April 1945|
|Primary user||Imperial Japanese Army Air Force|
Design and development
The Ki-87 was developed in response to American B-29 Superfortress raids on the Home Islands. It followed up on earlier research by Nakajima and the Technical Division of Imperial Army Headquarters into boosting a large radial engine with an exhaust-driven turbo-supercharger, which had begun in 1942, well before the B-29 raids began. The efforts of the Technical Division of Imperial Army Headquarters eventually culminated into the Tachikawa Ki-94-I, while the Ki-87 was developed as a fall-back project, using less stringent requirements. Nakajima started in July 1943 with the construction of three prototypes, to be completed between November 1944 and January 1945, and seven pre-production aircraft, to be delivered by April 1945. The Technical Division of Imperial Army Headquarters made itself felt during the development of the Ki-87 prototype when they insisted upon placing the turbo-supercharger in the rear-fuselage, and from the sixth prototype the Nakajima fighter was to have that arrangement. The Ki-87 had a rearward folding undercarriage to accommodate the storage of ammunition for the wing-mounted cannon in the wing. 
Construction was delayed due to problems with the electrical undercarriage and the turbo-supercharger, and the first prototype was not completed until February 1945; it first flew in April, but only five test flights were completed, all with the undercarriage in the extended position.
A further variant, the Ki-87-II, powered by a 3,000 hp Nakajima Ha217 (Ha-46) engine and with the turbo-supercharger in the same position as the P-47 Thunderbolt, never went further than the drawing board.
Production of 500 aircraft was planned, but the war ended before any more than the single prototype were built.
The sole completed prototype was in natural metal finish; some paintings show a black anti-glare area in front of the cockpit, but this is not seen on any of the known photographs of the plane.
Specifications (Ki-87 prototype)
- Crew: 1
- Length: 11.82 m (38 ft 9.375 in)
- Wingspan: 13.423 m (44 ft 0.5 in)
- Height: 4.503 m (14 ft 9.312 in)
- Wing area: 26.00 m² (279.860 ft²)
- Empty weight: 4,388 kg (9,672 lb)
- Loaded weight: 5,633 kg (12,416 lb)
- Max. takeoff weight: 6,102 kg (13,448 lb)
- Powerplant: 1 × Mitsubishi Ha219 Ru (Ha-44/11) eighteen-cylinder air-cooled radial four-blade, 1,789 kW (2,400 hp)
- Maximum speed: 697 km/h (379 kn, 433 mph)
- Cruise speed: 470 km/h (254 kn, 292 mph)
- Service ceiling: 12,855 m (42,175 ft)
- Wing loading: 216.6 kg/m² (44.3 lb/ft²)
- Power/mass: 0.317 kW/kg (2.3 kg/hp; 5.2 lb/hp)
- Guns: 2 × 30 mm (1.18 in) Ho-105 cannons in the outer wing panels and 2 × 20 mm synchronized Ho-5 cannons in the wing roots
- Bombs: 1 x 250 kg (550 lb) bomb under fuselage
- Aircraft of comparable role, configuration and era
- Green 1973, p. 90.
- Francillon 1979, p. 238 and 265.
- Green and Swanborough 1977, p. 62.
- Green and Swanborough 1977, p. 63.
- Francillon 1979, p. 239.
- Francillon 1979, p. 240.
- Green and Swanborough 1977, p. 64.
- FAOW 1976, pp. 59–61 and front cover.
- Green and Swanborough 1977, pp. 62–64.
- FAOW 1976, p. 67.
- Francillon, René J. Japanese Aircraft of the Pacific War. London, Putnam & Company, 1970 (Second edition 1979). ISBN 0-370-30251-6.
- Green, William. War Planes of the Second World War, Volume Three: Fighters. London: Macdonald, 1961 (Seventh impression 1973). ISBN 0-356-01447-9.
- Green, William and Swanborough, Gordon. WW2 Aircraft Fact Files: Japanese Army Fighters, part 2. London, Macdonald & Jane's, 1977. ISBN 0-354-01068-9.
- Unknown Author Famous Aircraft of the World, first series, no.76: Japanese Army Experimental Fighters (1). Japan: Bunrin-Do Co. Ltd., August 1976.
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