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Caproni Vizzola F.4

Military Aircraft

The Caproni Vizzola F.4 was an Italian fighter prototype designed in 1937 and built from 1939, a single-seat low-wing cantilever monoplane with retractable landing gear. It was developed in parallel with the Vizzola F.5 and shared its airframe, with design begun in late 1937 by a team led by F. Fabrizi, the F.4 standing for Fabrizi 4. The fuselage was welded steel tube covered with flush-riveted duralumin and the wing was wooden with a stressed plywood skin. Fabrizi intended an Isotta Fraschini Asso water-cooled engine, but the Air Ministry preferred that the Asso not be used in fighters, so the project was halted in favour of the radial-engined F.5. The last of 12 pre-production F.5 aircraft was later converted into the F.4 prototype with a German Daimler-Benz DB 601A, and the Regia Aeronautica assigned it to the 303a Squadriglia, which operated it experimentally in 1942.

Facts
Engine Class
Piston 1
Units Built
1 1
Top Speed (km/h)
550 1
Mass (kg)
2462 1
Maximum Mass (kg)
3000 1
Engine
Daimler-Benz DB 601A inverted V12 liquid-cooled piston engine 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Caproni Vizzola F.4 (Wikipedia)

Of Make

Source Caproni Vizzola F.4 (Wikipedia)
Sources
1. Caproni Vizzola F.4 (Wikipedia)
  • Lead
    was an Italian fighter aircraft prototype that was designed in 1937 and built from 1939
  • Operational history
    the lone F.4 prototype
  • Specifications (F.4)
    1 × Daimler-Benz DB 601A inverted V12 liquid-cooled piston engine
  • Specifications (F.4), top speed
    Maximum speed: 550 km/h (340 mph, 300 kn) at 3,750 m (12,300 ft)
  • Specifications (F.4), mass
    Empty weight: 2,462 kg (5,428 lb)
  • Specifications (F.4), maximum mass
    Gross weight: 3,000 kg (6,614 lb)
  • Lead, manufacturer
    The Caproni Vizzola F.4 was an Italian fighter aircraft prototype
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