Farman A.2
From Wikipedia, the free encyclopedia
The Farman A.2 was a 1920s French high-wing monoplane designed as a military reconnaissance and observation aircraft. Only one was built.[1]
Development
The open-cockpit tandem two-seat monoplane was displayed at the 1924 Paris Salon de l'Aeronautique.[1] It was designed to minimise drag and the wide-chord wing was faired into the top of the fuselage and the aircraft was carefully shaped.[1] The aircraft did not meet performance expectations and was scrapped.[1]
Specifications
Data from [1]
General characteristics
- Crew: 2 (pilot, observer)
- Length: 10.5 m (34 ft 5¼ in)
- Wingspan: 15.0 m (49 ft 2½ in)
- Empty weight: 1500 kg (3307 lb)
- Gross weight: 2500 kg (5512 lb)
- Powerplant: 1 × Farman 12-cylinder arrow piston engine, 373 kW (500 hp)
Performance
- Maximum speed: 220 km/h (137 mph)
- Service ceiling: 7000 m (22,965 ft)
- 4 × 0.303in (7.7mm) machine gun
References
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- Notes
- Bibliography
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
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