| 词条 | Aichi E16A | |||||||||||||||
| 释义 |
The Aichi E16A Zuiun (瑞雲 "Auspicious Cloud", Allied reporting name "Paul") was a two-seat reconnaissance seaplane operated by the Imperial Japanese Navy during World War II. Design and developmentThe Aichi E16A originated from a 1939 specification for a replacement for the Aichi E13A, which at that time had yet to be accepted by the Imperial Japanese Navy Air Service (IJNAS).[2] Disagreements about the requirements in the 14-Shi specification prevented most manufacturers from submitting designs, but in 1941 a new 16-Shi specification was drafted by the IJNAS around the Aichi AM-22 design which had already been made by Aichi engineers Kishiro Matsuo and Yasuhiro Ozawa.[2] The first AM-22, which first got the experimental designation Navy Experimental 16-Shi Reconnaissance Seaplane and later the short designation E16A1, was completed by May 1942 and was a conventional, low-wing monoplane equipped with two floats and had the unusual (for a seaplane) feature of being equipped with dive brakes, located in the front legs of the float struts, to allow it to operate in a secondary role as a dive bomber. Variants[3][4]
Initial named Experimental Type 14 two-seat reconnaissance seaplane (14試2座水上偵察機, 14-Shi 2-Za Suijō Teisatsuki). 3 prototypes produced. Mounted {{convert|1300|HP|abbr=on}} Mitsubishi MK8A Kinsei 51 engine, 2 × forward-firing 7.7 mm (.303in) Type 97 machine guns, 1 × rearward-firing 7.7 mm Type 92 machine gun.
General production model. Mounted {{convert|1300|HP|abbr=on}} Mitsubishi MK8N Kinsei 54 engine, 2 × forward-firing 20 mm Type 99-2 cannons, 1 × rearward-firing 13 mm Type 2 machine gun.
Initial named Zuiun Model 22. Single prototype with a {{convert|1560|HP|abbr=on}} Mitsubishi MK8P Kinsei 62 radial engine. One plane converted from E16A1, incomplete. Operators
Specifications (E16A1 Zuiun Model 11){{aircraft specifications|plane or copter?= plane |jet or prop?= prop |ref=Japanese Aircraft of the Pacific War[1] |crew= 2 (pilot and observer) |capacity= |length main= 10.83 m |length alt= 35 ft 6 in |span main= 12.81 m |span alt= 42 ft |height main= 4.79 m |height alt= 15 ft 9 in |area main= 28 m² |area alt= 300 ft² |airfoil= |empty weight main= 2,945 kg |empty weight alt= 6,490 lb |loaded weight main= 4,553 kg |loaded weight alt= 10,000 lb |useful load main= |useful load alt= |max takeoff weight main= |max takeoff weight alt= |more general= |engine (prop)= Mitsubishi Kinsei 54 |type of prop= 14-cylinder, air-cooled, twin-row radial engine |number of props= 1 |power main= 970 kw |power alt= 1,300 hp |power original= |max speed main= 439 km/h |max speed alt= 237 kn, 274 mph |cruise speed main= |cruise speed alt= |never exceed speed main= |never exceed speed alt= |stall speed main= |stall speed alt= |range main= 2,420 km |range alt= 1,307 nmi, 1,510 mi |ceiling main= 10,000 m |ceiling alt= 33,000 ft |climb rate main= 10 m/s |climb rate alt= 1,970 ft/min |loading main= 139.3 kg/m² |loading alt= 28.5 lb/ft² |power/mass main= 0.21 kW/kg |power/mass alt= 0.29 hp/kg; 0.13 hp/lb |more performance= |armament=
|avionics= }} See also{{aircontent|related= |similar aircraft=
|lists=
|see also= }} References
1. ^1 2 Francillon 1979, p. 287. 2. ^1 Francillon 1979, p. 284. 3. ^1 Bunrindō (1983), p. 110–111, p. 159–163 4. ^1 Bunrindō (1994), p. 8, p. 25, p. 71–77
External links{{commons category|Aichi E16A}}{{Aichi Aircraft}}{{Japanese Navy Reconnaissance seaplanes}}{{Allied reporting names}} 6 : Aichi aircraft|Japanese military reconnaissance aircraft 1940–1949|Floatplanes|Single-engined tractor aircraft|Low-wing aircraft|Aircraft first flown in 1942 |
|||||||||||||||
| 随便看 |
|
开放百科全书收录14589846条英语、德语、日语等多语种百科知识，基本涵盖了大多数领域的百科知识，是一部内容自由、开放的电子版国际百科全书。