Some information and background history -
(Resource Wikipedia)
Role Twin-engine reconnaissance aircraft
Manufacturer Mitsubishi
First flight September, 1939
Introduction July, 1941
Retired 1945
Primary user Imperial Japanese Army Air Force
Number built 1,742
The Mitsubishi Ki-46 was a twin-engine reconnaissance aircraft used by the Imperial Japanese Army in World War II. Its Army Shiki designation was Type 100 Command Reconnaissance Aircraft; the Allied nickname was "Dinah".
General characteristics
Crew: two (pilot and observer)
Length: 11.00 m (36 ft 1 in)
Wingspan: 14.70 m (48 ft 2¾ in)
Height: 3.88 m (12 ft 8¾ in)
Wing area: 32.0 m² (344 ft²)
Empty weight: 3,263 kg (7,194 lb)
Loaded weight: 5,050 kg (11,133 lb)
Max. takeoff weight: 5,800 kg (12,787 lb)
Powerplant: 2 × Mitsubishi Ha-102 Army Type 1 14-cylinder radial engines, 807 kW (1,080 hp) (take-off) each
Performance
Maximum speed: 604 km/h (326 knots, 375 mph) at 5,800 m (19,000 ft)
Cruise speed: 400 km/h (217 knots, 249 mph)
Range: 2,474 km (1,337 nmi, 1,537 mi)
Service ceiling: 10,720 m (35,200 ft)
Wing loading: 157.8 kg/m² (32.3 lb/ft²)
Climb to 8,000 m (26,250 ft): 17 min 58 sec
On 12 December 1937, the Imperial Japanese Army Air Force issued a specification to Mitsubishi for a long-range strategic reconnaissance aircraft to replace the Mitsubishi Ki-15. The specification demanded an endurance of six hours and sufficient speed to evade interception by any fighter in existence or development, but otherwise did not constrain the design by a team led by Tomio Kubo (a 1931 graduate from the Aeronautical Section of the Faculty of Engineering at Tokyo Imperial University) whose aesthetics are densely infused to this elegant aircraft.
The resulting design was a twin-engined, low-winged monoplane with a retractable tailwheel undercarriage. It had a small diameter oval fuselage which accommodated a crew of two, with the pilot and observer situated in individual cockpits separated by a large fuel tank. Further fuel tanks were situated in the thin wings both inboard and outboard of the engines, giving a total fuel capacity of 1,490 L (328 imperial gallons). The engines, two Mitsubishi Ha-26s, were housed in close fitting cowlings developed by the Aeronautical Research Institute of the Tokyo Imperial University to reduce drag and improve pilot view.
This aircraft was first used by the Japanese Army in Manchukuo and China, where seven units were equipped with it, and also at times by the Japanese Imperial Navy in certain reconnaissance missions over the northern coasts of Australia and New Guinea.
The Japanese Army used this aircraft for the same type of missions (which were not authorized) over present-day Malaysia during the months before the Pacific War. Later, it was used for high altitude reconnaissance over Burma, Indochina, Thailand, and the Indian Ocean. The Ki-46 was regarded by the British RAF in Burma as a difficult aircraft to counter, only occasionally intercepting them successfully. On September 25, 1944, Flying Officer Wittridge shot down a Ki-46, using a personally modified Spitfire Mk. 8. Wittridge had removed two machine guns and the seat armour, and also polished the wing leading edges to gain extra speed.[11]
In 1944-45, during the last days of the war, it was modified as a high-altitude interceptor, with two 20 mm cannon in the nose and one 37 mm (1.46 in) cannon in an "upwards-and-forwards" position - almost like the Luftwaffe 's Schräge Musik night fighter cannon emplacements - for fighting USAAF B-29 Superfortresses over the metropolitan Japanese islands. It lacked stability for sustained shooting of the 37 mm (1.46 in) weapon, had only a thin layer of armour plating, lacked self-sealing fuel tanks, and was slow to climb.
The Ki-46 was also assigned to two whole Sentai (wings/groups), as well as individual Chutaicho (junior operational commanders) in the Imperial Japanese Army Air Service, during the Pacific War.
The Allies captured some examples during the conflict which were then repaired and flown for evaluation purposes.
