Nakajima Ki-4

Ki-4
Nakajima Ki-4 (Army Type 94 Reconnaissance aircraft)
Role	Reconnaissance, Light Ground-Attack, Trainer, Target Tug
Manufacturer	Nakajima Aircraft Company
First flight	1933
Introduction	1934
Retired	1943
Primary users	IJA Air Force Manchukuo Air Force
Produced	516

The Nakajima Ki-4Kyūyon-shiki teisatsuki (九四式偵察機) was the last biplane reconnaissance aircraft of the Japanese Imperial Army. It saw combat service in Manchukuo and in north China during the early stages of the Second Sino-Japanese War.

Design and development

The Ki-4 was initially produced by Nakajima in response to a 1931 specification for a high-performance reconnaissance aircraft that could also be used in the light ground support role. After evaluating aircraft from Europe and the United States, the Imperial Japanese Army Air Force selected a new design by the domestic Nakajima Aircraft Company. The prototype was test flow in May 1934.

The Nakajima Ki-4 was a biplane design with staggered wings and fixed divided landing gear. It was powered by one 477 kW (640 hp) Nakajima Ha-8, nine-cylinder, air-cooled radial engine. Maximum speed was 300 km/h (190 mph) and maximum take-off weight 2,500 kg (5,510 lb). It was armed with up to four 7.7 mm (.303 in) machine guns, two fixed to fire forward, synchronized with the propeller, and one or two more mounted dorsally on a flexible mount. The maximum bomb load was 50 kg (110 lb).

A total of 516 units were produced, 333 by Nakajima between March 1934 and February 1939, and 57 under license by Tachikawa Aircraft Company Ltd and another 126 by Manshū in Manchukuo (Manchuria).

Operational history

The first Ki-4s began equipping Imperial Japanese Army Air Force units in 1935 and were an active part of Japanese fighter squadrons for a number of years thereafter. The Ki-4s saw substantial service in the early stages of the Second Sino-Japanese War from 1938. They also functioned as light ground-attack aircraft in the support of advancing Japanese ground troops. However, these biplanes were vulnerable to even the oldest and slowest moving enemy fighters. By the time of the entry of Japan into World War II, the Ki-4s were regarded as obsolete. A number were still retained for use in the supply and liaison role from 1941, and others were transferred to the Manchukuo Air Force, but those that had not been lost in service served briefly as elementary trainers or target tugs before being scrapped. All of the Ki-4s were removed from active service by 1943.

Two Ki-4s were tested as seaplanes, one with twin floats and the other with one main and two stabilizing floats, but neither version was placed into production.

Variants

• Ki-4 (Army Type 94 Reconnaissance Aircraft)

Operators

Japan

• Imperial Japanese Army Air Force

Manchukuo

• Manchukuo Air Force

Specifications (Ki-4)

Data from Japanese Aircraft, 1910–1941

General characteristics

• Crew: 2
• Length: 7.73 m (25 ft 4 in)
• Wingspan: 12 m (39 ft 4 in)
• Height: 3.5 m (11 ft 6 in)
• Wing area: 29.7 m² (320 sq ft)
• Empty weight: 1,664 kg (3,668 lb)
• Gross weight: 2,474 kg (5,454 lb)
• Powerplant: × Nakajima Ha8 (Army Type 94 550hp Air Cooled Radial) 9-cylinder air-cooled radial piston engine, 450–480 kW (600–640 hp)
• Propellers: 2-bladed controllable-pitch metal propeller

Performance

• Maximum speed: 153 km/h (95 mph, 83 kn) at 2,400 m (7,874 ft)
• Service ceiling: 8,000 m (26,000 ft)
• Time to altitude: 3,000 m (9,843 ft) in 9 minutes
• Wing loading: 82.5 kg/m² (16.9 lb/sq ft)
• Power/mass: 0.1826 kW/kg (0.1111 hp/lb)

Armament

• Guns: Up to 4× 7.7 mm (0.303 in) machine guns (2 fixed-forward firing synchronised and 1 or 2 on a flexible mount in the read cockpit)
• Bombs: 50 kg (110 lb){citation nedded

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|crew= 2 |capacity= |payload main= |payload alt= |length main= 7.73 m |length alt= 25 ft 4 in |span main= 12.00 m |span alt= 38 ft 4 in |height main= 3.50 m |height alt= 11 ft 5 in |area main= 29.7 m2 |area alt= 319.7 ft2 |airfoil= |empty weight main= 1,664 kg |empty weight alt= 3,668 lb |loaded weight main= 2,474 kg |loaded weight alt= 5,454 lb |useful load main= |useful load alt= |max takeoff weight main= 2,616 kg |max takeoff weight alt= 5,767 lb |more general= |engine (jet)= |type of jet= |number of jets= |thrust main= |thrust alt= |thrust original= |afterburning thrust main= |afterburning thrust alt= |engine (prop)= Nakajima Ha-8 |type of prop= nine-cylinder, air-cooled radial piston engine |number of props= 1 |power main= 477 kW at take-off |power alt= 640 hp |power original= , 560 kW (750 hp) at 4000 m (13,120 ft) |propeller or rotor?= |propellers= |number of propellers per engine= |propeller diameter main= |propeller diameter alt= |max speed main= 283 km/h at 2,400 m |max speed alt= 176 mph at 7,874 ft |cruise speed main= |cruise speed alt= |stall speed main= |stall speed alt= |never exceed speed main= |never exceed speed alt= |range main= 1,200 km |range alt= 745 mi |ceiling main= 8,000 m

See also

• List of military aircraft of Japan

References

Notes

Bibliography

• Francillon, Ph.D., René J. (1979). Japanese Aircraft of the Pacific War. London: Putnam & Company Ltd. ISBN 0-370-30251-6.
• Mikesh, Robert C.; Shorzoe Abe (1990). Japanese Aircraft, 1910-1941. Annapolis, MD: Naval Institute Press. ISBN 1-55750-563-2.

External links

• History of Nakajima Aircraft