Aviation of World War II |
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Ca.602
The Ca.602 owes its appearance to a competition announced by the DGCA and Regia Aeronautica on August 30, 1938. Then an acrobatic aircraft with high flight characteristics was required, on which military pilots could learn aerobatics. It was assumed that an aircraft of this level should have performed all aerobatics without any restrictions, mainly at altitudes up to 1000 meters. A special commission was formed, which made changes to the technical specifications at least twice (September 5, 1938 and October 11, 1939) and only on March 21, 1940, the requirements were finally formulated, one of the conditions of which was the use of Isotta Frascini engines "Beta" (6-cylinder, 280 hp) or CAN D.VIII (8-cylinder, 300 hp). As the main prize, the winning company received an order for a large batch of aircraft. Six companies participated in the competition, presenting the following fighter designs: Caproni-Vizolla CV.3, Caproni-Taliedo Ca.214, CANSA FC.11, IMAM Ro.71, Breda Ba.92 and Caproni-Predappio Ca.602. The first three immediately left the race, and the remaining ones were awarded an order for the construction of prototypes. It should be noted that not all companies fulfilled the requirement for engines, having included the Isottap Frascini "Gamma" (Ca.214) and Piaggio P.VIIZ (Ba.92) in the project. Ca.602 was considered one of the favorites. It was a two-seat biplane of mixed design equipped with an Alfa Romeo 115 engine with a two-blade propeller with a diameter of 2 meters. The fuselage of the aircraft was made of steel tubes and had a fabric covering; the two-spar wing was made entirely of wood and covered with plywood. The chassis was made non-retractable. In July 1940, the prototype Ca.602 entered testing at the research center in Guidonia. In parallel with this, the company developed a single-seat version of the aircraft, designated Ca.603.
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