The Aero A.20 was a biplane fighter aircraft built in Czechoslovakia in 1923. It was evaluated for Czechoslovak 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.
== Specifications (A.20) == General characteristics
Crew: 1 Length: 6.6 m (21 ft 8 in) Wingspan: 9.7 m (31 ft 10 in) Wing area: 23.3 m2 (251 sq ft) Empty weight: 784 kg (1,728 lb) Max takeoff weight: 1,080 kg (2,381 lb) Powerplant: 1 × Skoda-built Hispano-Suiza 8Fb V-8 water-cooled piston engine, 220 kW (300 hp) Performance
Maximum speed: 225 km/h (140 mph, 121 kn) Service ceiling: 7,500 m (24,600 ft) Rate of climb: 5.88 m/s (1,157 ft/min) Armament
Guns: 2× 7.7 mm (0.303 in) Vickers machine guns
See also
Related development
Aero A.18 Aero A.19
Related lists
List of fighter aircraft