Aero A.20
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| Aero A.20 | |
|---|---|
| Type | Fighter aircraft |
| Manufacturer | Aero Vodochody |
| Status | Did not enter production |
| Primary user | Czech Air Force |
| Produced | 1923 |
| Number built | 1 |
The Aero A.20 was a biplane fighter aircraft built in Czechoslovakia in 1923. It was evaluated for Czech Air Force service against Aero's competing A.18 and A.19 designs, a competition that the A.18 won, meaning that this aircraft never entered production, and only a single prototype was ever built.
[edit] Specifications (A.20)
General characteristics
- Crew: 1
- Length: 6.60 m (21 ft 8 in)
- Wingspan: 9.70 m (31 ft 10 in)
- Height: m (ft in)
- Empty weight: 784 kg (1,730 lb)
- Max takeoff weight: 1,080 kg (2,380 lb)
- Powerplant: 1× Skoda-built Hispano-Suiza 8b, 300 hp (220 kW)
Performance
- Maximum speed: 225 km/h (120 knots, 140 mph)
- Range: km (nm, mi)
- Service ceiling 7,500 m (25,000 ft)
- Rate of climb: 5.88 m/s (1,160 ft/min)
Armament
- Guns: 2× .303 in (7.70 mm) Vickers machine guns
[edit] See also
Related development
Related lists
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