Breda CC.20
| Breda CC.20 | |
|---|---|
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| Role | Heavy bomber |
| Manufacturer | Breda |
| Designer | Ing Arturo Crocco and Ing Julio Constance |
| First flight | 1929 |
| Primary user | Italy |
| Number built | 1 |
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A Breda Ba.19 trainer under the wing of the CC.20.
The Breda CC.20 was an Italian heavy bomber prototype of 1929 designed and built by the Breda company.
Design and development
Ing Arturo Crocco and Ing Julio Constance designed the CC.20 -- "CC" for the surnames of the two engineers -- which was Breda 's first monoplane bomber. It was a seven-seat trimotor mid-wing monoplane powered by three 373-kilowatt (500-horsepower) Isotta-Fraschini Asso ("Ace") engines. It had a powerful defensive armament of one 25-millimeter cannon and seven 7.7-millimeter (0.303-inch) machine guns.
The CC.20 prototype first flew in 1929. Test flights showed it to be very slow and to have a short range, and Breda abandoned the project.
Operators
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Specifications
General characteristics
- Crew: 7
- Wingspan: 42 m (137 ft 10 in)
- Empty weight: 7,700 kg (16,976 lb)
- Gross weight: 12,000 kg (26,455 lb)
- Powerplant: 3 × Isotta-Fraschini Asso V-12 liquid-cooled piston engines, 373 kW (500 hp) each
Performance
- Maximum speed: 185 km/h (115 mph; 100 kn)
- Cruising speed: 155 km/h (96 mph; 84 kn)
Armament
- 1 x 25-millimeter cannon
- 7 x 7.7-millimeter (0.303-inch) machine guns
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Wikimedia Commons has media related to Breda CC.20. |
Notes
References
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