| F.5 | |
|---|---|
| |
| Role | FighterType of aircraft |
| Manufacturer | Caproni |
| First flight | 19 February 1939 |
| Introduction | ca. 1939-1940 |
| Primary user | Regia Aeronautica (Italian Royal Air Force) |
| Number built | 13 plus 1 F.4 prototype |
| Variants | Caproni Vizzola F.4(precursor) Caproni Vizzola F.6 |
The Caproni Vizzola F.5 was an Italian fighter aircraft that was built by Caproni. It was a single-seat, low-wing cantilever monoplane with retractable landing gear.
Development
The F.5 was developed in parallel with the Caproni Vizzola F.4, with which it shared a common airframe. Design began in late 1937 by a team led by F. Fabrizi. The aircraft had a welded steel-tube fuselage and wooden wings; the fuselage was covered with flush-riveted duralumin, while the wing had a stressed plywood skin. The F.5 (standing for Fabrizi 5) had a two-row 14-cylinder Fiat A.74 R.C. 38 radial engine, unlike its cousin the F.4, which Fabrizi and his design team intended to be powered by a water-cooled engine. The F.4 project was not pursued immediately because the Italian Air Ministry held its proposed engine in disfavor, but development of the F.5 continued.
The F.5 prototype first flew on 19 February 1939. The aircraft displayed very high maneuverability during official testing, prompting an order for both a second prototype and 12 preproduction models. The last of the preproduction aircraft was selected for use as a prototype in a renewed F.4 program, but the rest of the F.5 order was delivered to the Regia Aeronautica (Italian Royal Air Force).
No F.5 production models were built as Caproni decided to produce the more developed Caproni Vizzola F.6M fighter instead.
Operational history
The Regia Aeronautica assigned the 11 preproduction F.5 fighters to the 300° Squadriglia, 51° Stormo for operational use. By 1942, they were serving as night fighters in the 167° Gruppo.
The F.5 was offered to foreign customers. It has been said that the Aeroplani Caproni subsidiary in Peru acquired the license rights for local manufacture, but no F.5s were ever built in Peru.
Variants
- F.5
- Prototype and preproduction aircraft, powered by a Fiat A.74 R.C. 38 radial engine, 13 built, plus a 14th airframe which was completed as the Caproni Vizzola F.4.
- F.5bis
- One re-engined F.5, powered with an 1175 h.p. Alfa Romeo R.A.I000 R.C.44-la Monsonie (Monsoon) (license-built DB 601A-l) engine.
- F.5 Gamma
- A one- or two-seat advanced trainer powered by a 540 h.p. Isotta Fraschini Gamma R.C.35 IS alr-cooled engine, armed with one 7.7-mm. Breda-SAFAT machine gun, with an estimated maximum speed of 254 m.p.h. Not proceeded with.
Operators
Specifications (F.5)
Data from Italian Civil and Military Aircraft 1930-1945
General characteristics
- Length: 7.90 m (25 ft 11 in)
- Wingspan: 11.3 m (37 ft 1 in)
- Height: 3 m (9 ft 10 in)
- Wing area: 17.6 m (189 sq ft)
- Empty weight: 1,850 kg (4,079 lb)
- Gross weight: 2,238 kg (4,934 lb)
- Powerplant: 1 × Fiat A.74 R.C.38 14-cyl. air-cooled radial piston engine, 649 kW (870 hp) at take-off
Performance
- Maximum speed: 510 km/h (320 mph, 280 kn)
- Range: 770 km (480 mi, 420 nmi) at 455 km/h (283 mph)
- Service ceiling: 9,500 m (31,200 ft)
- Time to altitude: 6,500m (21,325ft) in 6 min 30 s
Armament
- Guns: 2 × 12.7 mm (0.5 in) forward-firing Breda-SAFAT machine guns
See also
Aircraft of comparable role, configuration, and era
Notes
- ^ Thompson, Jonathan W. (1963). Italian Civil and Military aircraft 1930-1945. USA: Aero Publishers Inc. ISBN 0-8168-6500-0.
- ^ Green and Swanborough, p. 109
References
- Donald, David, ed. (1997). The Encyclopedia of World Aircraft. Prospero Books. p. 232. ISBN 1-85605-375-X.
- Garello, Giancarlo (June 2001). "La chasse de nuit italienne (1ère partie: les débuts)" [Italian Night Fighters: The Beginning]. Avions: Toute l'Aéronautique et son histoire (in French) (99): 19–24. ISSN 1243-8650.
- Green, William, and Gordon Swanborough. The Complete Book of Fighters: An Illustrated Encyclopedia of Every Fighter Aircraft Built and Flown. New York: SMITHMARK Publishers, 1994. ISBN 0-8317-3939-8.
