Mitsubishi Ki-46

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 and Jojo Hattori. 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. forces on October 3, 1945. Menado, Celebes. The first prototype aircraft, with the designation Ki-46, flew in November 1939 from the Mitsubishi factory at Kakamigahara, Gifu, north of Nagoya. Tests showed that the Ki-46 was underpowered, and slower than required, only reaching rather than the specified . Otherwise, the aircraft tests were successful. Because the type was still faster than the Army's latest fighter, the Nakajima Ki-43, as well as the Navy's new A6M2, an initial production batch was ordered as the Army Type 100 Command Reconnaissance Plane Model 1 (Ki-41-I). Although at first the Ki-46 proved almost immune from interception, the Imperial Japanese Army Air Force realised that improved Allied fighters such as the Supermarine Spitfire and P-38 Lightning could challenge this superiority, and in July 1942, it instructed Mitsubishi to produce a further improved version, the Ki-46-III. This had more powerful, fuel-injected Mitsubishi Ha-112 engines, and a redesigned nose, with a fuel tank ahead of the pilot and a new canopy, smoothly faired from the extreme nose of the aircraft, eliminating the "step" of the earlier versions. The single defensive machine gun of the earlier aircraft was omitted not long into the production run. The new version first flew in December 1942, demonstrating significantly higher speed at . The performance of the Ki-46-III even proved superior to that of the aircraft intended to replace it (the Tachikawa Ki-70), which as a result did not enter production. During operational testing in March 1944, it was discovered that replacing the engines' single exhaust collector ring with individual pipes provided extra thrust and an increase in top speed to . In an attempt to yet further improve the altitude performance of the Ki-46, two prototypes were fitted with exhaust driven turbosupercharged Ha-112-II-Ru engines. This version first flew in February 1944, but only two prototypes were built. Mitsubishi factories made a total of 1,742 examples of all versions (34 x Ki-46-I, 1093 x Ki-46-II, 613 x Ki-46-III, 4 x Ki-46-IV) from 1941 to 1944. ==Operational history==

based at Kallang display the tail fin of a Mitsubishi Ki-46 which they shot down over Johore, Malaya, on 10 January 1942 , 1944 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 VIII. Wittridge had removed two machine guns and the seat armour and also polished the wing leading edges to gain extra speed. The leading American fighter pilot Richard Bong, flying a P-38 Lightning, managed to shoot down a Ki-46 over the coast of Papua New Guinea in late 1942. In 1944–45, during the last days of the war, it was modified as a high-altitude interceptor, with two 20 mm cannons in the nose and one 37 mm (1.46 in) cannon in an "upwards-and-forwards" position, almost like the Luftwaffes 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. The Ki-46 III was the only Japanese aircraft type sent to the NII VVS Soviet Air Force Test Institute for evaluation during 1946–7. ==Variants==

(note:- The Shiki designations must be used in full, as written below, because the Type number only refers to the year of the designs inception.) ; Army Type 100 Command Reconnaissance Plane: The Shiki designation for the Ki-46 Command Reconnaissance Plane ; Army Type 100 Air Defence Fighter:The Shiki designation for the Ki-46 Interceptor Fighter ; Army Type 100 Assault Plane:The Shiki designation for the Ki-46 Assault Plane ; Ki-46: Prototype. ; Ki-46 I: Reconnaissance version of the Ki-46. ; Ki-46 II: The first operational model of the series. ; Ki-46 II KAI: Three-seat training version of the Ki-46. Used for radio and navigation training, with a redesigned cabin, dorsal en echelon extension. Conversions of the Ki-46 II. ; Ki-46 III: "Traditional" stepped windshield replaced with a smooth, curved, glazed panel extended over the pilot's seat giving a more aerodynamic nose profile. Engine power increased to 1,500 hp (Ha-112-II), extra fuel tank added in the nose. ; Ki-46 III-KAI: Defense interceptor/night fighter version of the Ki-46. Equipped with two 20 mm cannon in the nose and one 37 mm (1.46 in) cannon in the "Schräge Musik"-style upwards-aimed dorsal frontal position. ; Ki-46 III: Land strike version of the Ki-46, without 37 mm (1.46 in) cannon armament. ; Ki-46 IIIb: Ground-attack version. ; Ki-46 IIIc: Unbuilt design project. ; Ki-46 IV: Prototype, equipped with two turbocharged 1,119 kW (1,500 hp) Mitsubishi Ha-112-IIru engines, and more fuel capacity. ; Ki-46 IVa/b: Series models of reconnaissance/fighter aircraft, unbuilt design projects ==Operators==

; • French Air Force – Captured aircraft. ; • Imperial Japanese Army Air Force • Imperial Japanese Navy Air Service ; • Chinese Communist Air Force Two captured Ki-46s in communist Chinese hands served as a ground-attack aircraft and a trainer respectively, and the last Ki-46 retired in the early 1950s. ==Surviving aircraft==

The only complete survivor is a Ki-46-III Army Type 100 example, that is part of the collection of the Royal Air Force Museum in the United Kingdom. Built around 1943, it was part of the 81st Sentai, 3rd Chutai IJAAF. This unit had detachments deployed across the South West Pacific. It became part of the RAF St Athan collection of historic aircraft, before moving to the Royal Air Force Museum Cosford in 1989. Ownership was transferred from the Ministry of Defence to the RAF Museum in 1998 Wreckage of a Ki-46-II, abandoned at Jacquinot Bay Airfield, was recovered in 2003. ==Specifications (Ki-46-II)==