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https://en.wikipedia.org/wiki/Yokosuka_D4Y
The Yokosuka (???) D4Y Suisei (?? "Comet") Navy Carrier dive bomber was operated by the Imperial Japanese Navy. Its Allied reporting name was "Judy". The D4Y was one of the fastest dive bombers of the war and only the delays in its development hindered its service while its predecessor, the slower fixed-gear Aichi D3A, remained in service much longer than intended. Despite limited use, the speed and the range of the D4Y were nevertheless valuable, and the type was used with success as reconnaissance aircraft as well as for kamikaze missions. Development of the aircraft began in 1938 at the Yokosuka Naval Air Technical Arsenal as a carrier-based dive bomber to replace the Aichi D3A. The aircraft was a single-engine, all-metal low-wing monoplane, with a wide-track retractable undercarriage and wing-mounted dive brakes. It had a crew of two: a pilot and a navigator/radio-operator/gunner, seated under a long, glazed canopy which provided good all-round visibility. The pilot of bomber versions was provided with a telescopic bombsight. The aircraft was powered by an Aichi Atsuta liquid-cooled inverted V12 engine, a licensed copy of the German DB 601, rated at 895 kW (1,200 hp). The radiator was behind and below the three-blade propeller, as in the P-40 Warhawk. The aircraft had a slim fuselage that enabled it to reach high speeds in horizontal flight and in dives, while it had excellent maneuverability despite high wing loading, with the Suisei having superior performance to contemporary dive bombers such as the Curtiss SB2C Helldiver. In order to conform with the Japanese Navy's requirement for long range, weight was minimized by not fitting the D4Y with self-sealing fuel tanks or armour. In consequence, the D4Y was extremely vulnerable and tended to catch fire when hit. Early versions of the D4Y were difficult to keep operational because the Atsuta engines were unreliable in front-line service. From the beginning, some had argued that the D4Y should be powered by an air-cooled radial engine which Japanese engineers and maintenance crew had experience with, and trusted. The aircraft was re-engined with the reliable Mitsubishi MK8P Kinsei 62, a 14-cylinder two-row radial engine as the Yokosuka D4Y3 Model 33. Although the new engine improved ceiling and rate of climb (over 10,000 m/32,800 ft, and climb to 3,000 m/9,800 ft in 4.5 minutes, instead of 9,400 m/30,800 ft and 5 minutes), the higher fuel consumption resulted in reduced range and cruising speed and the engine obstructed the forward and downward view of the pilot, hampering carrier operations. These problems were tolerated because of the increased availability of the new variant. Role Dive bomber Manufacturer Yokosuka First flight December 1940 Introduction 1942 Retired 1945 Primary user Imperial Japanese Navy Air Service Produced 1942–1945 Number built 2,038 Lacking armor and self-sealing fuel tanks, the Suiseis did not fare well against Allied fighters. They did, however, cause considerable damage to ships, including the carrier USS Franklin which was nearly sunk by an assumed single D4Y and the light carrier USS Princeton which was sunk by a single D4Y. The D4Y was faster than the A6M Zero and some were employed as D4Y2-S night fighters against Boeing B-29 Superfortress bombers late in the war. The night fighter conversions were made at the 11th Naval Aviation Arsenal at Hiro. Each D4Y2-S had its bombing systems and equipment removed, and replaced by a 20 mm Type 99 cannon installed in the rear cockpit, with the barrel slanted up and forwards in a similar manner to the German Schräge Musik armament fitting (pioneered by the IJNAS in May 1943 on the Nakajima J1N). Some examples also carried two or four 10 cm air-to-air rockets under the wings; lack of radar for night interceptions, inadequate climb rate and the B-29's high ceiling limited the D4Y2-S effectiveness as a night fighter. Little is known of their operations. At the end of the war, D4Ys were still being used operationally against the U.S. Navy. Among the last of these were 11 aircraft led by Vice Admiral Matome Ugaki on a search mission on 15 August 1945, of which all but three were lost. Specifications (D4Y2) General characteristics Crew: two (pilot & gunner/radio operator) Length: 10.22 m (33 ft 6 in) Wingspan: 11.50 m (37 ft 9 in) Height: 3.74 m (12 ft 3 in) Wing area: 23.6 m² (254 ft²) Empty weight: 2,440 kg (5,379 lb) Loaded weight: 4,250 kg (9,370 lb) Powerplant: 1 × Aichi Atsuta AE1P 32 liquid-cooled inverted V12 piston engine, 1,400 hp (1,044 kW) Performance Maximum speed: 550 km/h (342 mph) Range: 1,465 km (910 mi) Service ceiling: 10,700 m (35,105 ft) Rate of climb: 14 m/s (2,700 ft/min) Wing loading: 180 kg/m² (37 lb/ft²) Power/mass: 0.25 kW/kg (0.15 hp/lb) Armament 2× forward-firing 7.7 mm Type 97 aircraft machine guns 1× rearward-firing 7.92 mm Type 1 machine gun 500 kg (1,102 lb) of bombs (design), 800 kg (1,764 lb) of bombs (kamikaze) * |
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