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Fiat C.R.42 : ウィキペディア英語版
Fiat CR.42

The Fiat CR.42 ''Falco'' ("Falcon", plural:''Falchi'') was a single-seat sesquiplane fighter that served primarily in Italy's ''Regia Aeronautica'' before and during World War II. The aircraft was produced by Fiat Aviazione, and entered service, in smaller numbers, with the air forces of Belgium, Sweden and Hungary. With more than 1,800 built, it was the most widely produced Italian aircraft to take part in World War II.〔''Avions militaires 1919-1939 - Profils et Histoire''1979, p. 89.〕 The Fiat CR.42 was the last of the Fiat biplane fighters to enter front line service, and represented the epitome of the type, along with the Gloster Gladiator.
RAF Intelligence praised its exceptional manoeuvrability, further noting that "the plane was immensely strong",〔Haining 2005, pp. 8, 15.〕 though it stood little chance against faster, more heavily armed monoplanes.〔Wheeler 1992, p. 50.〕 It performed at its best with the Hungarian Air Force on the Eastern Front, where it had a kill to loss ratio of 12 to 1.〔Skulski 2007, p. 67.〕
==Design and development==

The CR.42 was an evolutionary design based on the earlier Fiat CR.32, which was in turn derived from the Fiat CR.30 series created in 1932. The ''Regia Aeronautica'' had employed the CR.32 during the Spanish Civil War with great success, which led to Fiat proposing a more advanced fighter based around the supercharged Fiat A.74R1C.38 air-cooled radial engine geared to drive a metal three-blade Fiat-Hamilton Standard 3D.41-1 propeller of diameter and a robust, clean, sesquiplane design. The rigidly braced wings covered with fabric were constructed from light duralumin alloy and steel. It reached a top speed of 438 km/h (272 mph) at 5,300 m (17,400 ft) and 342 km/h (213 mph) at ground level. Climb rate was 1 minute and 25 seconds to 1,000 m (3,280 ft) and of 7 minutes and 20 seconds to 6,000 m (19,700 ft).〔Sgarlato 2005〕
In spite of the biplane configuration, the CR.42 was a modern, "sleek-looking" design based around a strong steel and alloy frame incorporating a NACA cowling housing the radial engine, with fairings for the fixed main landing gear. The CR.42's upper wing was larger than its lower wing, a configuration known as a sesquiplane.〔Sgarlato 2005〕 The aircraft proved exceptionally agile thanks to its very low wing loading, although at the same time, the CR.42 lacked armour and radio equipment.
During evaluation, the CR.42 was tested against the Caproni Ca.165 biplane fighter, and was judged to be superior, although the Ca.165 was a more modern design which boasted a higher speed at the cost of maneuverability. Although the age of the biplane was coming to an end a number of other air forces expressed interest in the new fighter, and a number of early Falcos were delivered to foreign customers.
Soon after its combat introduction, Fiat developed a number of variants. The CR.42bis and CR.42ter had increased firepower, the CR.42N was a night fighter, the CR.42AS was optimised for ground attack, and the CR.42B ''Biposto'' was a two-seat trainer.〔Taylor 1969, p. 212.〕
The ''Biposto'' was the most extensively modified, with a longer fuselage allowing a second seat to be placed in tandem. About 40 aircraft were produced by Agusta and Caproni Trento. Its length was increased by 68 centimeters over the standard fighter, to a total of to 8.94 m; the height was 23 centimeters less. Empty weight was only more, as the wheel fairings had been removed. Overall weight was 2,300 kg. Top speed was 430 km/h at 5,300 meters, only 8 km/h less. Up to 1945, two machine guns were fitted.〔Sgarlato, Nico.''Fiat CR.42''〕
Experimental configurations included the I.CR.42 (''Idrovolante''= seaplane) and the CR.42DB. Beginning in 1938, Fiat had worked on the I.CR.42, then gave the task to complete the project to CMASA factory in Marina di Pisa on the Tirreno sea coast. The only prototype was built in 1940. Tests started at the beginning of 1941, at the Vigna di Valle base, on Lake Bracciano, north of Rome. Top speed was 423 km/h, range was 950 km while ceiling was reduced to 9,000 m. Empty weight went from , full weight from .
The CR.42DB was an attempt to improve the type's performance by installing a Daimler-Benz DB 601 V12 engine of 753 kW (1,010 hp).〔Taylor 1969, pp. 212–213.〕 This prototype, MM 469), was flown by test pilot Valentino Cus in March 1941, over Guidonia Montecelio, near Rome. This variant could reach a top speed of 518 km/h (323 mph), with a maximum ceiling of and a range of . The project was cancelled as the biplane configuration did not offer any advantages over contemporary monoplane fighter designs. Although it never went into production, to this day the variant has the distinction of being the fastest biplane ever flown.〔Lopez, Donald S. ''Aviation: A Smithsonian Guide''. Washington, DC: Ligature Inc., 1995.〕
It is still not certain how many CR.42s were built. The most likely estimate is 1,819 in total, including the 63 (51 according to some sources) produced under ''Luftwaffe'' control and the 140 produced for export.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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